JP2003286804A - Engine combined with variety of entire rotor blade steam gas turbine - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To prevent global warming by approximating the exhaust temperature of a gas turbine to -273°C and sorting and collecting water and water vapour by condensation using cryogenic combustion gas as a core, and by converting the turbine into the drive of an internal combustion engine of zero-exhaust-combustion gas and one third electric fee or the like because it is urgently necessary to prevent the global warming. <P>SOLUTION: An engine transfers the heat of combustion by a combustor and a heat exchanger in an engine combined with an entire rotor blade steam gas turbine as much as possible. It has approximately twice as a heat collecting amount as a conventional boiler does by approximating the exhaust temperature of the combustion gas to -273°C and collecting the substantially overall quantity of heat more than -273°C in compressed air. A process, which increases the collected heat to the generated amount of idea ranging from 220 times to 530 times as much as a traditional gas turbine (idea generated amount = generated amount of quantity of heat of combustion gas + generated amount of mass of combustion gas), is adapted so as to be simple in construction and to consume the minimum quantity of heat as rapidly making frictional loss between water 1700 times of gravity power small by means of a turbine blade with water repellency annularly casted every section, and is adapted so as to discern as a hail and droplet, of water by condensing moisture making the cryogenic combustion gas as the core, and is configured to be the engine combined with a entire rotor blade steam gas turbine which is zero-exhaust-combustion gas such as CO2, etc. <P>COPYRIGHT: (C)2004,JPO

Description

【発明の詳細な説明】Detailed Description of the Invention

【０００１】[0001]

【発明の属する技術分野】本発明はアイディアを数字で
説明する、例えば最先端再熱蒸気タービンの再熱を逆転
して、水噴射過熱蒸気を冷却し、大気圧重力パワー最先
端再熱蒸気タービンの１７００倍や、真空部１００００
倍の、水質量を最適最大として、動翼面積の一部乃至大
部分を既存蒸気発電の大気圧部１／１７００や、真空部
１／１００００等に縮小した、設計容易な全動翼蒸気タ
ービン等とします。そして撥水性噴口８３を含む撥水性
タービン翼８１の全動翼とし、摩擦損失を最小として略
直線蛇行的に噴射して機械効率を上昇する、各種全動翼
蒸気ガスタービン合体機関として、既存ボイラの２倍回
収熱量の（水蒸気熱量出力＝真空部既存技術の１０００
０倍重力パワー／〆×２倍回収熱量×５倍落差×２乃至
３倍機械効率）＝（既存ガスタービンの２２０乃至５３
０倍アイディア発電量）等に関する。FIELD OF THE INVENTION The present invention describes the idea numerically, for example by reversing the reheat of a state-of-the-art reheat steam turbine to cool water-injected superheated steam and atmospheric gravity power state-of-the-art reheat steam turbine. 1700 times, or vacuum section 10000
Double-rotating steam turbine with double the water mass as the optimum maximum and reducing part or most of the blade area to the atmospheric pressure part 1/1700 of the existing steam power generation, the vacuum part 1/10000, etc. And so on. Then, as all moving blades of the water-repellent turbine blade 81 including the water-repellent injection port 83, the friction loss is minimized and the injection is performed in a substantially linear meandering manner to increase the mechanical efficiency. 2 times the recovered heat quantity (steam heat quantity output = 1000 in the vacuum part existing technology)
0 times gravity power / 〆 × 2 times recovered heat quantity × 5 times head × 2 to 3 times mechanical efficiency) = (220 to 53 of existing gas turbine)
0 times idea generation amount) etc.

【０００２】本発明は全動翼タービン翼を、加熱高温・
撥水性金属・撥水性物質の被覆・撥水性セラミックス・
撥水性加工の、何れか１以上で構成の撥水性タービン翼
にすることで、撥水性タービン翼８１と水等との間の摩
擦損失を低減して、全動翼により略直線蛇行的に噴射し
て、摩擦損失最小・消費熱量最少で出力を発生して、機
械効率を２乃至３倍に上昇します。構造が大幅に小型簡
単大出力の、全動翼蒸気ガスタービンや全動翼ガスター
ビンや全動翼蒸気タービンとして、水質量の重力パワー
大気圧部１７００倍、真空部では既存蒸気タービンの１
００００倍等として、効率良く出力を得るため、水蒸気
や燃焼ガスの保有熱量を、水噴射冷却して凝縮水や水質
量の速度エネルギに変換して、重力パワー増大により、
出力を効率良く増大する技術に関する。In the present invention, a full-rotor turbine blade is heated at a high temperature
Water-repellent metal, water-repellent substance coating, water-repellent ceramics,
By making the water-repellent turbine blade of any one or more of water-repellent finishes, the friction loss between the water-repellent turbine blade 81 and water etc. is reduced, and the jetting is performed in a substantially linear meandering manner by all moving blades. Then, the output is generated with the minimum friction loss and the minimum heat consumption, and the mechanical efficiency is increased by 2 to 3 times. The structure is significantly small, simple, and large-power, as a full-blade steam gas turbine, a full-blade gas turbine, and a full-blade steam turbine.
In order to obtain an efficient output, such as 0000 times, the retained heat quantity of steam and combustion gas is converted into velocity energy of condensed water and water mass by water injection cooling, and by increasing the gravity power,
The present invention relates to a technique for efficiently increasing output.

【０００３】本発明は全動翼圧縮機翼を、撥水性金属・
撥水性物質の被覆・撥水性セラミックス・撥水性加工
の、何れか１以上で構成の撥水性水冷却翼８７にするこ
とで、撥水性水冷却翼８７と水等との間の摩擦損失を低
減して、全動翼により略直線蛇行的に空気圧縮して、摩
擦損失最小で空気を水冷却して圧縮し、燃焼器兼熱交換
器に供給します。そして燃焼ガス質量と燃焼ガス熱量は
別物であるため、各種全動翼ガスタービン乃至全動翼蒸
気ガスタービンの、燃焼器兼熱交換器により限りなく燃
焼熱交換し、熱力学を逆転して、燃焼ガス入口温度を最
低とし、燃焼ガス排気温度を−２７３℃に近付けます。
すると圧縮空気保有熱量−２７３℃以上略全部を含め
て、燃料発熱量全部を熱回収して、既存ボイラの２倍前
後の熱回収量の燃焼ガス熱量として、例えば全動翼蒸気
タービン等を駆動します。そして燃焼ガス質量により全
動翼ガスタービン等を駆動の過程を、燃焼ガス消費熱量
０以下も可能とし、該熱効率を無限上昇に近付ける技術
に関する。In the present invention, the rotor blade compressor blade is made of a water-repellent metal
Reduction of friction loss between the water-repellent water cooling blade 87 and water by using the water-repellent water cooling blade 87 composed of any one or more of coating of water-repellent substance, water-repellent ceramics, and water-repellent finish. Then, the air is compressed in a substantially straight line meandering manner by all moving blades, and the air is cooled by water with minimum friction loss to be compressed and supplied to the combustor and heat exchanger. And since the combustion gas mass and the combustion gas heat quantity are different things, the combustion heat exchange is endless by the combustor and heat exchanger of various all-blade gas turbines or all-blade steam gas turbines, and thermodynamics is reversed, Set the combustion gas inlet temperature to the minimum and bring the combustion gas exhaust temperature close to -273 ° C.
Then, the entire amount of heat generated by the fuel, including substantially all of the compressed air retained calorie −273 ° C. or higher, is recovered, and the combustion gas calorie of about twice the heat recovery amount of the existing boiler is used to drive, for example, a full-blade steam turbine. To do. Further, the present invention relates to a technology that makes it possible to drive the moving blade gas turbine or the like by the mass of combustion gas even if the heat consumption of combustion gas is 0 or less, so that the thermal efficiency approaches an infinite increase.

【０００４】本発明は、燃焼器兼熱交換器により限りな
く燃焼熱交換して得た、最低温度の燃焼ガス質量を、既
存ガスタービンの２倍落差×４倍質量等として、全動翼
蒸気ガスタービンに供給します。出力を発生の過程でも
水噴射燃焼ガスを可能な限り冷却して、燃焼ガス容積を
縮小して水蒸気や凝縮水を増大し、燃焼ガス排気温度を
−２７３℃に近付けます。即ち既存ガスタービンのよう
な高温排気温度では、ＣＯ２等燃焼ガス排気０が不可能
です。そこで全重力パワー等の出力を増大すると共に、
断熱膨張極低温燃焼ガスを核に凝縮水や水蒸気を凝集し
て、自然現象と同様に雹や水滴等とすることで、全動翼
蒸気ガスタービン合体機関の、燃焼ガス排気０を可能に
する技術に関する。According to the present invention, the combustion gas mass at the lowest temperature obtained by endless combustion heat exchange by the combustor / heat exchanger is set as a double head × 4 times the mass of the existing gas turbine. Supply to gas turbine Even in the process of generating power, the water-injected combustion gas is cooled as much as possible, the volume of combustion gas is reduced, steam and condensed water are increased, and the exhaust temperature of combustion gas approaches -273 ° C. That is, at the high exhaust gas temperature of existing gas turbines, it is impossible to exhaust combustion gas such as CO2. Therefore, while increasing the output such as total gravity power,
Adiabatic expansion cryogenic combustion gas is used as a core to condense condensed water and water vapor to form hail and water droplets as in the case of natural phenomena, enabling zero combustion gas exhaust of a combined rotor and steam gas turbine engine. Regarding technology.

【０００５】本発明は既存再熱蒸気タービンのように、
超臨界圧力過熱蒸気から真空圧力まで、１００００倍以
上に膨張させると、真面目な設計は不可能です。そこで
燃料の種類を問わず、更に微粉炭燃焼等も追加して、燃
焼器兼熱交換器により限りなく燃焼熱交換して得た、既
存ボイラの２倍前後の全回収熱量を、超臨界圧力等の水
蒸気として、全動翼蒸気タービンの最上流側に供給して
出力を発生します。出力発生の全過程で水噴射手段から
の水噴射により、水蒸気を冷却して、気化潜熱を含む大
部分の水蒸気速度を、大気圧重力パワーが水蒸気の１７
００倍の水質量速度にエネルギ変換し、全重力パワーを
最適最大とすることで、動翼面積の一部乃至大部分を既
存再熱蒸気タービンの、大気圧部１／１７００や真空部
１／１００００等に縮小して、真面目な設計が可能な動
翼面積にする技術に関する。The present invention, like existing reheat steam turbines,
Supercritical pressure When superheated steam to vacuum pressure is expanded 10,000 times or more, serious design is impossible. Therefore, regardless of the type of fuel, pulverized coal combustion is also added, and the total amount of heat recovered about twice that of the existing boiler obtained by endless combustion heat exchange with the combustor and heat exchanger is supercritical pressure. The steam is supplied to the most upstream side of the full-blade steam turbine to generate output. Water vapor is cooled by the water jetting means in the whole process of output generation to cool most of the steam velocity including latent heat of vaporization, and the atmospheric gravity power is 17
By converting energy to water mass velocity of 00 times and maximizing the total gravity power to the optimum maximum, a part or most of the blade area is reduced to the atmospheric pressure part 1/1700 and the vacuum part 1 / of the existing reheat steam turbine. The present invention relates to a technology for reducing the blade area to 10,000 or the like to obtain a moving blade area that allows a serious design.

【０００６】本発明は、燃焼ガス排気を０としてＣＯ２
等を排気しないため、回転出力の輸送機器用等として
は、極低温燃焼ガス用凝縮水を最大にするため、全動翼
蒸気タービン＋全動翼ガスタービン＝全動翼蒸気ガスタ
ービンとして使用します。従って飛行機等の場合は高空
を噴射推進する過程で、極低温燃焼ガスを核に雹や水滴
を凝集生成して、海中等に投下して燃焼ガス排気を０に
します。船舶等では極低温燃焼ガスを含む雹や水滴等と
して分別し、選択して直接海水を４℃等に冷却して、Ｃ
Ｏ２等を海底に沈殿させます。陸上輸送機器等でも極低
温燃焼ガスを含む雹や水滴として分別したり、化学物質
混入によりＣＯ２等を合成溶解排水して、輸送用機器か
ら、ＣＯ２等公害ガス排気を０に近付ける技術に関す
る。In the present invention, the combustion gas exhaust gas is set to 0 and CO 2 is discharged.
Since it does not exhaust air etc., it is used as a full-power blade steam turbine + full-blade gas turbine = full-blade steam gas turbine in order to maximize condensed water for cryogenic combustion gas for transportation equipment with rotary output. I will. Therefore, in the case of airplanes, in the process of injecting and propelling high altitudes, the extremely low temperature combustion gas is used as the nucleus to agglomerate hail and water droplets, which are dropped into the sea or the like to eliminate combustion gas exhaust. In ships, etc., it is separated into hail and water droplets containing cryogenic combustion gas, and selected to directly cool seawater to 4 ° C, etc.
Precipitate O2 etc. on the sea floor. The present invention relates to a technique for separating land-based transportation equipment and the like into hail and water droplets containing cryogenic combustion gas, and chemically dissolving and discharging CO2 and the like by mixing chemical substances to bring emissions of pollutant gases such as CO2 to zero from transportation equipment.

【０００７】本発明は、燃焼ガス排気を０としてＣＯ２
等を排気しないため、噴射推進出力の輸送機器用等とし
ては、燃焼器兼熱交換器により限りなく燃焼熱交換して
得た、超臨界圧力等の水蒸気の一部により、全動翼圧縮
機を含む全動翼蒸気タービンを駆動して、残りの水蒸気
の一部及び燃焼ガス全部を、夫々霧吹きの原理を利用し
てバイパス噴射推進し、残りの水蒸気を燃焼器兼熱交換
器乃至過熱蒸気溜に貯蔵しておき、適宜に使用する噴射
推進出力の各種輸送機器等とします。そして回転出力や
噴射推進出力を利用する、各種航空機、各種船舶、各種
車両、各種熱と電気と冷熱の供給設備、電気の供給設備
等あらゆる用途に対応可能にして、磁気摩擦動力伝達装
置も適宜に含めた新技術の、各種全動翼蒸気ガスタービ
ン合体機関に関する。In the present invention, the combustion gas exhaust gas is set to 0 and CO2
Since it does not exhaust gas etc., it is used for transportation equipment of injection propulsion output, etc., by using a part of steam such as supercritical pressure obtained by endless combustion heat exchange with a combustor and heat exchanger, Drive all-blade steam turbine including, and part of the remaining steam and all of the combustion gas are bypass-injected and propelled using the principle of atomization, and the remaining steam is combustor / heat exchanger or superheated steam. It is stored in a reservoir and used as various types of transportation equipment with injection and propulsion output for proper use. And it can be used for various applications such as various aircraft, various ships, various vehicles, various heat and electricity and cold heat supply equipment, electricity supply equipment, etc. that utilize rotation output and injection propulsion output, and magnetic friction power transmission device is also appropriate. The present invention relates to various types of all-blade steam gas turbine integrated engines of the new technology.

【０００８】[0008]

【従来の技術】蒸気タービン・ガスタービン複合機関の
うち、ガスタービン燃焼器の内部に熱交換器を設けた先
行技術として特開昭５０−８９７３７号が開示されてい
る。この発明は、ガスタービン燃焼器の高温領域に、蒸
気タービンサイクルの過熱器乃至再熱器を設けることに
よって、特別の補助的な燃焼器を必要とすることなく、
蒸気タービンサイクルの過熱蒸気温度を高め、複合プラ
ント全体の効率向上を図るものである。又、特開昭５２
−１５６２４８号は、ガスタービン間の燃焼ガスとの熱
交換によって蒸発を行なうことにより、廃熱回収ボイラ
出口廃ガス温度の低下を図り、ボイラ効率を向上させる
ことが開示されている。しかし、これらは、いずれも過
給ボイラサイクルの熱効率の向上を図るもので、ガスタ
ービンの圧力比と比出力の同時上昇を図るものでもガス
タービンの熱効率上昇を図るものでもない。2. Description of the Related Art Among steam turbine / gas turbine combined engines, Japanese Patent Laid-Open No. 50-89737 is disclosed as a prior art in which a heat exchanger is provided inside a gas turbine combustor. The present invention, by providing the superheater or reheater of the steam turbine cycle in the high temperature region of the gas turbine combustor, without the need for a special auxiliary combustor,
The superheated steam temperature of the steam turbine cycle is raised to improve the efficiency of the entire complex plant. In addition, JP-A-52
No. 156248 discloses that evaporation is performed by heat exchange with combustion gas between gas turbines to reduce the temperature of waste gas at the exit of the waste heat recovery boiler and improve boiler efficiency. However, these are all intended to improve the thermal efficiency of the supercharged boiler cycle, and are not intended to simultaneously increase the pressure ratio and the specific output of the gas turbine or the thermal efficiency of the gas turbine.

【０００９】又、先の出願としてガスタービン燃焼器を
改良した、特願平６−３３０８６２号、特願平７−１４
５０７４号、特願平７−３３５５９５号、特願平８−４
１９９８号、特願平８−８０４０７号、特願平８−１４
３３９１号、特願平８−２０４０４９号、特願平８−２
７２８０６号、特願平９−１０６９２５号、特願平９−
１８１９４４号、特願平１０−１３４７２０号、特願平
１０−１３４７２１号、特願平１１−６９４０６号、特
願平１１−７７１８９号、特願平１１−１０６３２９
号、特願平１１−１１７４０４号、特願平１１−１３２
０８３号、特願２０００−０２４５５２号、特願２００
０−０３２５３９号、特願２０００−０４３７０６号、
特願２０００−０５８０７９号、特願２０００−１０７
４４６号、特願２０００−３９２４０１号、特願２００
１−０１１３９９号、特願２００１−０１５２３４号、
特願２００１−０２０９６３号、特願２００１−１７１
１２８号、特願２００１−３１２３３８号、特願２００
１−３３６１３９号があります。以上先の出願に基づく
優先権主張出願は概略的に、全動翼を含む及び／ガスタ
ービンの全複数の燃焼器を、熱交換器としても兼用し
て、限りなく燃焼熱交換して、燃焼ガス入り口温度を低
下させることにより、燃焼ガス熱量と燃焼ガス質量を、
別々に使用可能とし、過熱蒸気や燃焼ガスを水噴射冷却
して、大気圧重力パワー１７００倍の凝縮水を最適最大
とするものです。As a prior application, Japanese Patent Application No. 6-330862 and Japanese Patent Application No. 7-14 have improved the gas turbine combustor.
No. 5074, Japanese Patent Application No. 7-335595, Japanese Patent Application No. 8-4
1998, Japanese Patent Application No. 8-80407, Japanese Patent Application No. 8-14
3391, Japanese Patent Application No. 8-204049, Japanese Patent Application 8-2
72806, Japanese Patent Application No. 9-106925, Japanese Patent Application No. 9-
No. 181944, Japanese Patent Application No. 10-134720, Japanese Patent Application No. 10-134721, Japanese Patent Application No. 11-69406, Japanese Patent Application No. 11-77189, Japanese Patent Application No. 11-106329.
Japanese Patent Application No. 11-117404, Japanese Patent Application No. 11-132
083, Japanese Patent Application 2000-024552, Japanese Patent Application 200
No. 0-032539, Japanese Patent Application No. 2000-043706,
Japanese Patent Application No. 2000-058079, Japanese Patent Application No. 2000-107
No. 446, Japanese Patent Application No. 2000-392401, Japanese Patent Application 200
No. 1-011399, Japanese Patent Application No. 2001-015234,
Japanese Patent Application No. 2001-020963, Japanese Patent Application No. 2001-171
128, Japanese Patent Application No. 2001-312338, Japanese Patent Application 200
There is 1-336139. The priority application based on the above-mentioned application is generally composed of all the plurality of combustors including all moving blades and / or gas turbines, which are also used as heat exchangers for endless combustion heat exchange and combustion. By lowering the gas inlet temperature, the combustion gas heat quantity and combustion gas mass
It can be used separately, and the superheated steam and combustion gas are jetted and cooled by water to maximize the condensed water with an atmospheric pressure gravity power of 1700 times.

【００１０】[0010]

【発明が解決しようとする課題】既存最先端再熱蒸気タ
ービン発電技術に関し、再三再熱して過熱蒸気容積を増
大し、重力パワーを低減して明らかに風力発電にしてお
ります。又再熱蒸気タービンと同様に、水力発電の水を
途中で加熱して１７００倍の水蒸気にしても、落差×質
量に変化が無く、加熱熱量＋容積増大は全部損失となり
ます。そして重力パワーは大気圧部で水の１／１７００
に、真空部では１／１００００等減少するため、風力発
電と同様に動翼面積を１７００倍や、１００００倍等に
増大が必要です。即ち、超臨界圧力過熱蒸気等として大
きな落差を設定すると、断熱膨張では１００００倍以上
に容積が増大し、重力パワーが減少するため、動翼面積
も１００００倍に近い増大が必要です。即ち、設計不可
能な動翼面積のため、膨大な静翼を設けて多段に堰き止
めて風向きを反転させ、実用過熱蒸気速度に減速する、
無茶苦茶設計となり、１／１００発電量等に低減して大
損失になります。[Problems to be solved by the invention] Regarding the existing cutting-edge reheat steam turbine power generation technology, we are rewinding repeatedly to increase the volume of superheated steam and reduce the gravity power to make wind power clearly. Also, like the reheat steam turbine, even if the water of the hydroelectric power plant is heated halfway and steamed 1700 times, there is no change in the head x mass, and the heating heat + volume increase is all lost. And gravity power is 1/1700 of water at atmospheric pressure.
In addition, since the vacuum part decreases by 1/10000, it is necessary to increase the blade area by 1700 times or 10000 times, similar to wind power generation. In other words, if a large head is set as supercritical pressure superheated steam, the volume will increase 10,000 times or more in adiabatic expansion, and the gravity power will decrease, so the blade area must also increase nearly 10,000 times. That is, because of the impractical design of the blade area, a huge number of stationary blades are installed to block in multiple stages to reverse the wind direction and reduce the speed to a practical superheated steam speed.
The design is unreasonable, and the power generation is reduced to 1/100, resulting in a large loss.

【００１１】既存最先端ガスタービン発電技術で最も愚
かな誤りは、燃焼ガス入口温度を上昇して、燃焼ガス容
積を増大し、燃焼ガス速度の上昇により、発電量や出力
を上昇増大すると言うのが常識ですが、燃焼ガス入口温
度の上昇は有害設計事項で、タービンの耐熱限界温度の
上昇を必要として、利益皆無の全熱量の熱損失です。燃
焼ガス容積の増大も有害設計事項で、単位重力パワーの
減少により、タービン動翼面積の増大と通路断面積の増
大が必要で、怠れば重力パワーの減少分が速度増大とな
り、速度増大分が摩擦損失増大になります。既存最先端
の常識は、熱損失の基礎研究も皆無、燃焼ガス質量の基
礎研究も皆無、燃焼ガス熱量の基礎研究も皆無の、熱力
学妄信思考停止の最も愚かな誤りです。The most stupid mistake in the existing state-of-the-art gas turbine power generation technology is that the combustion gas inlet temperature is increased to increase the combustion gas volume, and the combustion gas velocity is increased to increase the power generation amount and output. It is common sense, however, that the rise in the combustion gas inlet temperature is a harmful design item, and the rise in the heat-resistant limit temperature of the turbine is required, which is a total heat loss with no profit. Increasing the combustion gas volume is also a harmful design matter.It is necessary to increase the turbine blade area and increase the passage cross-sectional area by decreasing the unit gravity power. If not, the decrease in gravity power results in an increase in speed, and the increase in speed is Friction loss will increase. The existing common sense is that there is no basic research on heat loss, no basic research on combustion gas mass, and no basic research on combustion gas calorific value, which is the most stupid mistake in stopping thermodynamic delusion thinking.

【００１２】既存最先端ガスタービン発電技術では、Ｃ
Ｏ２等を排気して地球温暖化を加速します。そこで全動
翼ガスタービン＋全動翼蒸気タービン＝全動翼蒸気ガス
タービンとします。そして全動翼蒸気ガスタービンの最
上流に、燃焼ガス熱量の超臨界圧力水蒸気等を供給し、
出力発生の全過程で水噴射水蒸気を冷却してその容積を
縮小し、蒸気速度や気化潜熱の大部分を水質量の速度エ
ネルギに変換し、大気圧重力パワー既存技術の１７００
倍等の水質量を最大にします。するとタービン動翼面積
の一部乃至大部分を、大気圧部１／１７００や真空部１
／１００００以下に、縮小が可能になります。即ち、超
臨界圧力から断熱膨張させて、１００００倍以上に容積
を増大すると、通常設計不可のため、タービンの動翼面
積を、通常設計容易な面積に縮小して、大気圧重力パワ
ー１７００倍水質量による、タービン翼の動圧駆動が最
大の急務です。In the existing state-of-the-art gas turbine power generation technology, C
It exhausts O2 and accelerates global warming. Therefore, we will use full-blade gas turbine + full-blade steam turbine = full-blade steam gas turbine. Then, the supercritical pressure steam of the combustion gas calorie is supplied to the most upstream of the all-blade steam gas turbine,
In the entire process of generating power, the water jet steam is cooled to reduce its volume, and most of the steam velocity and latent heat of vaporization are converted into velocity energy of water mass.
Maximize double water mass. Then, a part or most of the turbine moving blade area is reduced to the atmospheric pressure part 1/1700 and the vacuum part 1
It can be reduced to less than 10,000. That is, when adiabatic expansion is performed from supercritical pressure to increase the volume by 10,000 times or more, it is usually impossible to design, so the turbine blade area is reduced to an area that is usually easy to design, and the atmospheric gravity power is 1700 times water. Dynamic pressure drive of turbine blades by mass is the most urgent task.

【００１３】有限の燃料資源を子孫にも残すため、発電
用には安価微粉炭燃料の特定燃焼にします。燃焼器兼熱
交換器で限りなく燃焼熱交換して、燃焼ガス入口温度を
最低にすることで、燃焼ガス排気温度を−２７３℃に近
づけ、燃焼灰の重力パワーにより全重力パワーを更に増
大して、燃焼ガス質量発電量を増大し、有限の燃料資源
を最も合理的に配分使用します。そして圧縮空気保有熱
量も含めて、既存ボイラの２倍前後の燃焼ガス熱量の回
収とし、燃焼器兼熱交換器により、超臨界圧力等の水蒸
気に変換して使用します。そして同一燃料燃焼ガス質量
（燃料熱量０以下）出力を（既存ガスタービンの２倍落
差×２倍乃至３倍機械効率×燃焼灰を含め２倍質量）＝
８倍乃至１２倍燃焼ガス質量発電量を狙う。[0013] In order to leave a finite fuel resource for descendants, a low-powder pulverized coal fuel is used for specific combustion for power generation. Combustion heat exchange with the combustor as much as possible to minimize the combustion gas inlet temperature, the combustion gas exhaust temperature close to -273 ℃, further increase the total gravity power by the gravitational power of combustion ash Increase the combustion gas mass power generation and use the finite fuel resources most reasonably. Then, the amount of heat of combustion gas, including the amount of heat possessed by compressed air, is about twice that of the existing boiler, and it is converted to steam at supercritical pressure by a combustor and heat exchanger for use. And the same fuel combustion gas mass (fuel calorific value 0 or less) output (2 times the head of the existing gas turbine × 2 to 3 times the mechanical efficiency × 2 times the mass including the combustion ash) =
Aim for 8 to 12 times combustion gas mass power generation.

【００１４】公害低減・地球温暖化防止も急がれます。
そこで例えば、極低温燃焼ガスを含む微粉炭燃焼灰を核
に、水蒸気や凝縮水等水分を凝集して、自然現象と同様
に雹や水滴として分別回収が最も容易な、全動翼蒸気ガ
スタービン合体機関として、又は全動翼蒸気タービンと
霧吹きの原理を併用した全動翼蒸気ガスタービン合体機
関として、燃焼ガス全部と残りの水蒸気をバイパス噴射
して使用します。そして分別回収した極低温燃焼ガスや
燃焼灰を含む雹等の冷熱は、水道水を冷却して都市部を
丸ごと冷却したり、海水を冷却して冷熱を海底に供給す
る過程で、海中生物に必要な酸素等を吸引して供給し、
海上輸送船舶や飛行機等を含めて、最も利用されていな
い海域での食料を増産が必要です。同様に公害発生源及
び地球温暖化源の自動車等、陸上輸送機器からのＣＯ２
等排気０が急がれます。It is urgent to reduce pollution and prevent global warming.
Therefore, for example, a pulverized coal combustion ash containing ultra-low temperature combustion gas is used as a core to agglomerate moisture such as steam and condensed water, and as with natural phenomena, it is the easiest to separate and collect as hail and water droplets. It is used as a combined engine or as a combined blade steam gas turbine combined engine that uses the principle of mist blowing together with the rotating blade steam turbine, by injecting all the combustion gas and the remaining steam by bypass. The cold heat of hail, etc., containing cryogenic combustion gas and combustion ash that have been separated and collected, can be transferred to marine organisms in the process of cooling tap water to cool the entire city area or cooling seawater to supply cold heat to the seabed. Suction and supply necessary oxygen etc.,
It is necessary to increase food production in the least-used water areas, including ocean shipping vessels and airplanes. Similarly, CO2 from land transportation equipment such as automobiles and other sources of pollution and global warming
Equal exhaust 0 is urgent.

【００１５】[0015]

【課題を解決するための手段】アイディアを明快に説明
するため数字で説明しますが、数字に限定するものでは
無い。最先端再熱蒸気タービンの再熱を逆転して、水噴
射過熱蒸気を冷却して、蒸気温度速度や気化潜熱を水質
量速度重力パワーに変換し、大気圧重力パワー水蒸気の
１７００倍水質量を最大として、動翼面積の一部乃至大
部分を、既存再熱蒸気タービン発電の１／１７００や、
真空部１／１００００以下に縮小して、通常の設計が容
易な全動翼蒸気タービンを含む、各種全動翼蒸気ガスタ
ービン合体機関にします。そして撥水性噴口８３を含む
全動翼撥水性タービン翼８１の、加熱高温・撥水性金属
・撥水性物質の被覆・撥水性セラミックス・撥水性加工
の、何れか１以上で構成の撥水性全動翼にすることで、
撥水性タービン翼８１と水質量等との間の摩擦損失を最
小に近付けて、機械効率を２乃至３倍に上昇し、同一燃
料量の発電量乃至出力を、既存技術の１００倍以上等と
した、各種全動翼蒸気ガスタービン合体機関のアイディ
アを提供します。各種発電所や各種自動車や各種船舶や
各種飛行機等として、実用化の過程で水質量パワーを最
大にし、ＣＯ２等燃焼ガス排気０等を可能にします。[Means for Solving the Problem] The explanation will be given with numbers to explain the idea clearly, but the idea is not limited to numbers. The reheat of the most advanced reheat steam turbine is reversed, the water injection superheated steam is cooled, the steam temperature velocity and the latent heat of vaporization are converted into water mass velocity gravity power, and the water mass is 1700 times the water pressure of atmospheric gravity power steam. As a maximum, part or most of the blade area is 1/1700 of the existing reheat steam turbine power generation,
The vacuum section is reduced to 1/10000 or less, and it becomes a combined engine of all moving blade steam gas turbines, including all moving blade steam turbines that are easy to design normally. Further, the water-repellent full-movement of any one or more of heating high temperature, water-repellent metal, coating of water-repellent metal, water-repellent substance, water-repellent ceramics, and water-repellent treatment of all rotor blades and water-repellent turbine blades 81 including the water-repellent nozzles 83. By making it a wing,
The friction loss between the water-repellent turbine blade 81 and the water mass is brought close to the minimum, the mechanical efficiency is increased by 2 to 3 times, and the power generation amount or output of the same fuel amount is 100 times or more of the existing technology. We will provide the idea of various all moving blade steam gas turbine integrated engine. For various power plants, various automobiles, various ships, various airplanes, etc., it maximizes the water mass power in the process of practical application and enables zero combustion gas exhaust such as CO2.

【００１６】既存最先端ガスタービン発電技術で最も愚
かな誤りは、逆転で最良になるため、全動翼ガスタービ
ンや全動翼蒸気ガスタービンの燃焼器を、熱交換器と兼
用して限りなく燃焼熱交換して、燃焼ガス入口温度を最
低に逆転します。すると燃焼温度と容積の障壁が最低と
なり、圧縮圧力を２倍以上の１０ＭＰａ以上として、理
論空燃比まで燃料燃焼質量の略４倍増が可能です。そこ
で空気圧縮の過程では、全動翼圧縮機を撥水性水冷却翼
８７で構成し、撥水性金属・撥水性物質の被覆・撥水性
セラミックス・撥水性加工の、何れか１以上で構成の撥
水性全動翼にすることで、撥水性水冷却翼８７と水等と
の間の摩擦損失を最小に近付けて、燃焼器兼熱交換器で
限りなく燃焼熱交換します。熱交換して得た超臨界圧力
等の水蒸気熱量は、圧縮した空気の−２７３℃以上略全
部を含めて、同一燃料量既存ボイラの２倍前後の回収熱
量になります。同様に全動翼蒸気ガスタービンや全動翼
ガスタービンの、燃焼ガス入口温度を最低にすること
で、出力発生の過程では水噴射水蒸気を冷却して、水蒸
気速度や気化潜熱を水質量の速度パワーにエネルギ変換
して、出力を大幅に増大し、燃焼ガスによる水蒸気の冷
却を僅少にし、極低温燃焼ガス冷熱を最大等にします。
燃焼ガス排気温度は−２７３℃に近付け、極低温燃焼ガ
スを核に水分を凝集して、自然現象と同様に雹や水滴と
して分別可能にし、燃焼ガス排気０を可能にして、地球
温暖化防止します。Since the most stupid mistake in existing cutting-edge gas turbine power generation technology is best in reverse rotation, the combustor of a full-blade gas turbine or a full-blade steam gas turbine can be used as a heat exchanger without limit. Combustion heat exchange is performed to reverse the combustion gas inlet temperature to the minimum. Then, the barrier between combustion temperature and volume becomes the minimum, and the compression pressure is doubled to 10 MPa or more, and it is possible to increase the fuel combustion mass to approximately 4 times the stoichiometric air-fuel ratio. Therefore, in the process of air compression, the total moving blade compressor is composed of the water-repellent water cooling blades 87, and any one or more of the water-repellent metal / water-repellent substance coating / water-repellent ceramics / water-repellent finish is used. By using water-based full-rotor blades, the friction loss between the water-repellent water cooling blade 87 and water is brought to a minimum, and combustion heat is exchanged infinitely with the combustor and heat exchanger. The heat quantity of steam such as supercritical pressure obtained by heat exchange is about twice as much as that of the existing boiler with the same fuel quantity including almost all of -273 ° C or higher of compressed air. Similarly, by minimizing the temperature of the combustion gas inlet of all moving blade steam gas turbines and all moving blade gas turbines, the water injection steam is cooled in the process of power generation, and the steam speed and the latent heat of vaporization are converted to the speed of the water mass. Energy is converted to power, output is greatly increased, cooling of steam by combustion gas is made minimal, and cryogenic combustion gas cold heat is maximized.
Combustion gas exhaust temperature approaches -273 ° C, water is condensed by using extremely low temperature combustion gas as a core, and it can be separated as hail and water droplets like natural phenomenon, enabling combustion gas exhaust 0 and preventing global warming. To do.

【００１７】全部回転出力の場合、全動翼ガスタービン
＋全動翼蒸気タービン＝全動翼蒸気ガスタービンとし、
全動翼蒸気ガスタービンの最上流に、燃焼器兼熱交換器
で熱交換して得た燃焼ガス熱量を、超臨界圧力等の水蒸
気として供給し、出力発生の全過程で水噴射水蒸気を冷
却して容積を縮小し、蒸気速度や気化潜熱の大部分を水
質量速度パワーにエネルギ変換し、大気圧重力パワー既
存技術の１７００倍の水質量を最大にします。中流最適
段に燃焼ガス質量を最低温度の燃焼ガスとして供給し、
更に水噴射冷却して撥水性タービン動翼面積の一部乃至
大部分を、大気圧部１／１７００や真空部１／１０００
０以下に縮小します。即ち、タービンの動翼面積を、通
常設計が可能な面積に縮小することで、各種全動翼を可
能にし、大量の水を含む水蒸気や燃焼ガスを略直線蛇行
的に噴射して、撥水性タービン翼と水等との間の摩擦損
失を最小にし、機械効率を２乃至３倍に上昇します。In the case of full rotation output, full rotor gas turbine + full rotor steam turbine = full rotor steam gas turbine,
The combustion gas heat quantity obtained by heat exchange in the combustor and heat exchanger is supplied as steam at supercritical pressure to the most upstream of the all-blade steam gas turbine, and the water-injected steam is cooled in the entire process of output generation. It reduces the volume and converts most of steam velocity and latent heat of vaporization into water mass velocity power, and maximizes the water mass 1700 times the atmospheric pressure gravity power existing technology. Supply the mass of combustion gas as the lowest temperature combustion gas to the optimal middle stage,
Further, by water-cooling the water-repellent turbine, a part or most of the water-repellent turbine blade area is removed from the atmospheric pressure part 1/1700 and the vacuum part 1/1000.
Reduce to 0 or less. That is, by reducing the blade area of the turbine to an area that can be normally designed, various rotor blades are made possible, and steam and combustion gas containing a large amount of water are injected in a substantially linear meandering manner to repel water. Minimize friction loss between turbine blades and water, and increase mechanical efficiency 2-3 times.

【００１８】有限の燃料資源を子孫にも残すため、発電
用には安価微粉炭燃料の特定燃焼とし、燃焼灰の重力パ
ワーにより全重力パワーを更に増大して、燃焼ガス質量
発電量を増大し、有限の燃料資源を最も合理的に配分使
用します。燃焼器兼熱交換器で限りなく燃焼熱交換し
て、燃焼ガス入口温度を最低にする過程を、安価微粉炭
燃料の特定燃焼にし、燃焼ガス排気温度を−２７３℃に
近づけて、圧縮空気保有熱量−２７３℃以上略全部を含
めて、既存ボイラの２倍前後の燃焼ガス熱量の回収と
し、燃焼器兼熱交換器により超臨界圧力等の水蒸気に変
換して使用します。そして同一燃料燃焼ガス質量出力を
（既存ガスタービンの２倍落差×２倍乃至３倍機械効率
×燃焼灰を含め２倍質量）＝８倍乃至１２倍燃焼ガス質
量発電量とします。そして燃焼ガス熱量発電量＝（既存
ガスタービンの５倍落差×２倍乃至３倍機械効率×２倍
燃焼ガス熱量×１００００倍重力パワー／〆）＝２２０
倍乃至５３０倍燃焼ガス熱量発電量とします。そして全
動翼蒸気ガスタービン合体機関既存ガスタービンの２２
８倍乃至５４２倍アイディア発電量にします。In order to leave a finite fuel resource to the descendants, a specific combustion of inexpensive pulverized coal fuel is used for power generation, and the total gravity power is further increased by the gravity power of the combustion ash to increase the combustion gas mass power generation amount. , Use the limited fuel resources most reasonably. Combustion heat exchange with the combustor and heat exchanger as much as possible, the process of minimizing the combustion gas inlet temperature is specified combustion of inexpensive pulverized coal fuel, the combustion gas exhaust temperature is brought close to -273 ℃, compressed air possession The amount of heat, which is about -273 ° C or more, is recovered, and the amount of heat of combustion gas is about twice that of the existing boiler. It is used by converting it to steam at supercritical pressure using a combustor and heat exchanger. And the same fuel combustion gas mass output is (2 times the head of the existing gas turbine x 2 to 3 times the mechanical efficiency x 2 times the mass including the combustion ash) = 8 to 12 times the combustion gas mass power generation amount. And combustion gas calorie power generation amount = (5 times the head of existing gas turbine x 2 to 3 times mechanical efficiency x 2 times combustion gas calorific value x 10000 times gravity power / 〆) = 220
Double to 530 times the calorific value of combustion gas. And all rotor blade steam gas turbine combined engine 22 of existing gas turbine
8 to 542 times the idea power generation.

【００１９】回転出力は蒸気速度や気化潜熱の大部分
を、水質量の速度重力パワーにエネルギ変換容易な、全
動翼蒸気タービンで主として回転出力に変換し、電力や
自動車等の回転出力のみでは、燃焼ガス質量も回転出力
に変換し、燃焼ガス質量出力は極低温として水分を凝集
し、雹や水滴として分別回収可能として、燃焼ガス排気
を０とし、公害低減・地球温暖化防止に対応します。噴
射推進でも全動翼蒸気タービン回転出力により全動翼圧
縮気を駆動し、残りの水蒸気と燃焼ガス全部は、霧吹き
の原理を利用してバイパス噴射し、最も効率良く噴射推
進します。分別回収した雹や水滴等の冷熱は、水道水を
冷却して都市部を丸ごと冷却したり、海水を冷却して冷
熱を海底に供給する過程で、海中生物に必要な酸素等を
吸引して供給し、海域で人為的に魚類等の食料増産を図
ります。又海上輸送船舶や飛行機等を含めて、最も利用
されていない海域での食料増産を図り、公害発生源及び
地球温暖化源の自動車等、陸上輸送機器からのＣＯ２等
排気を０に近づけるため、同様に極低温燃焼ガスを核に
凝集した雹等と、燃焼ガスの１００倍質量以上等の水と
合流回収し、ＣＯ２等燃焼ガス排気を０に近付けます。The rotary output is obtained by converting most of the steam velocity and latent heat of vaporization into rotary output by a full-rotating blade steam turbine, which can easily convert energy into velocity gravity power of water mass. The combustion gas mass output is also converted to rotational output, and the combustion gas mass output is cryogenic, which condenses water and can be separated and collected as hail and water droplets. I will. Even in injection propulsion, all moving blade steam turbine rotation output drives all moving blade compressed air, and the remaining steam and all combustion gas are bypass-injected using the principle of atomization, and the most efficient injection propulsion is performed. Cold heat such as hail and water droplets collected separately is cooled by tap water to cool the entire city area, or in the process of cooling seawater and supplying cold heat to the seabed, by sucking oxygen etc. necessary for marine organisms. We will supply and artificially increase the production of food such as fish in the sea area. In addition, in order to increase food production in the least used sea areas, including ocean shipping vessels and airplanes, and to reduce CO2 emissions from land transportation equipment such as automobiles and other sources of pollution sources and global warming sources to zero, In the same way, the hail etc. that aggregated the cryogenic combustion gas in the nucleus and the water that is 100 times the mass of the combustion gas or more are combined and collected, and the exhaust gas of CO2 and other combustion gases approaches zero.

【００２０】[0020]

【発明の実施の形態】発明の実施の形態や実施例を、図
面を参照して説明するが、実施形態や実施例と、既説明
と後述部分と、その構成が略同じ部分には、同一の名称
又は符号を付して、後述するなどその重複説明はできる
だけ省略し、特徴的な部分や説明不足部分は、順次追加
重複説明する。又、発明の意図する所及び予想を具体的
に明快に説明するため、アイディアを数字で説明する部
分がありますが、数字に限定するものではありません。
又、この発明により最も簡単に効率良く空気を冷却圧縮
し、熱回収して低温空気と回収熱を使用する、燃焼器兼
熱交換器４は、既に特許出願済の燃焼器兼熱交換器を、
用途に合わせて選択使用します。又、極低温燃焼ガスや
凝縮水等で、最も効率良く出力を発生させるため、先の
発明の、加熱高温手段７９含た撥水性タービン翼としま
す。全動翼については、公知技術を含めます。燃焼ガス
排気温度を−２７３℃に近付けるアイディアは、極低温
燃焼ガスとし、−２７３℃は可能な最低温度として使用
します。BEST MODE FOR CARRYING OUT THE INVENTION Embodiments and examples of the present invention will be described with reference to the drawings. The duplicated description thereof will be omitted as much as possible, such as by adding the name or reference numeral of FIG. Also, in order to clearly explain the intended place and expectation of the invention, there are some parts where ideas are explained by numbers, but the ideas are not limited to numbers.
Further, according to the present invention, the combustor / heat exchanger 4 which cools and compresses the air in the simplest and efficient manner and uses the low temperature air and the recovered heat to recover heat is the combustor / heat exchanger already patented. ,
Select and use according to the application. Also, in order to generate the output most efficiently with extremely low temperature combustion gas, condensed water, etc., the water repellent turbine blade including the heating high temperature means 79 of the previous invention is used. All moving blades include publicly known technology. The idea to bring the exhaust temperature of the combustion gas close to -273 ° C is to use the cryogenic combustion gas, and -273 ° C is used as the lowest possible temperature.

【００２１】図１の全動翼ガスタービンの実施例に於い
て、全動翼圧縮機の主要部分の、外側圧縮機動翼群１６
及び内側圧縮機動翼群１７の撥水性水冷却翼８７を、冷
却手段５５により通水して水冷却し、その水を水噴射手
段５６より水噴射して、圧縮空気を直接接触冷却し、補
給水として熱回収し、空気容積を縮小します。全動翼と
することで翼間隔を増大した全動翼翼形として、圧縮空
気を略直線蛇行的に効率良く圧縮する、水との摩擦損失
を低減の、撥水性金属・撥水性物質の被覆・撥水性セラ
ミックス・撥水性加工の、何れかの撥水性水冷却翼８７
で成る、外側圧縮機動翼群１６及び内側圧縮機動翼群１
７を、段落毎圧縮機翼を環状に一体鋳造８４して、全自
動加工が可能及び組立構造可能とし、組立環状接続部で
冷却手段５５の水路を連結して、該組立環状接続部付近
に水噴射手段５６を設けます。冷却手段５５の水路は、
１以上複数又は段落全部又は段落半分の撥水性水冷却翼
８７を冷却後に、水噴射手段５６より水噴射して直接空
気冷却し、最も効率良く水冷却して空気圧縮します。熱
回収した高温補給水及び低温圧縮空気により、燃焼器兼
熱交換器で限りなく燃焼熱交換熱回収して、燃焼ガス入
口温度を可能な限り低下させて、熱回収量を最大に増大
し、燃焼ガス単位重力パワーを可能な限り上昇し、燃焼
ガス排気温度を−２７３℃に近付けます。In the embodiment of the all-blade gas turbine shown in FIG. 1, the outer compressor rotor blade group 16 is a main part of the all-blade compressor.
And the water-repellent water cooling blades 87 of the inner compressor moving blade group 17 are water-cooled by passing water by the cooling means 55, and the water is jetted by the water jetting means 56 to directly cool the compressed air and replenish it. It recovers heat as water and reduces the air volume. As a full-rotor blade airfoil whose blade spacing is increased by using full-rotor blades, it efficiently compresses compressed air in a substantially linear meandering manner, reduces friction loss with water, and coats water-repellent metals and water-repellent substances. Water-repellent ceramic / water-repellent processed water-repellent water cooling blade 87
An outer compressor blade group 16 and an inner compressor blade group 1
7, the compressor blade for each paragraph is integrally cast 84 to enable fully automatic processing and assembly structure, and the water passage of the cooling means 55 is connected by the assembled annular connecting portion to close the assembled annular connecting portion. Water injection means 56 will be provided. The water channel of the cooling means 55 is
After cooling one or more or a plurality of or all or half of the water-repellent water cooling blades 87, water is jetted from the water jetting means 56 for direct air cooling, and water is most efficiently cooled for air compression. With the high temperature makeup water and the low temperature compressed air that have recovered heat, the combustion heat exchange heat is recovered infinitely in the combustor and heat exchanger, the combustion gas inlet temperature is lowered as much as possible, and the heat recovery amount is increased to the maximum. Increase the combustion gas unit gravity power as much as possible to bring the combustion gas exhaust temperature close to -273 ° C.

【００２２】燃焼ガス入口温度を最低にして燃焼ガス排
気温度を−２７３℃に近付け、温度と容積の障壁を最低
にし、圧縮圧力を既存ガスタービンの略２倍の、１０Ｍ
Ｐａ以上を可能とし、燃料燃焼質量も理論空燃比まで、
既存ガスタービンの略４倍燃料燃焼とし、熱交換して得
た最低温度の燃焼ガスを、（既存ガスタービンの２倍落
差×同一燃焼ガス質量×２倍乃至３倍機械効率）＝（既
存ガスタービンの４倍乃至６倍の同一燃焼ガス質量出
力）とした全動翼ガスタービンとします。出力発生の初
期過程では水噴射燃焼ガス１０の冷却も含めて、燃焼ガ
ス容積を縮小して水質量を増大し、大気圧単位重力パワ
ーが１７００倍等に増大した水や燃焼ガス１０と、加熱
高温・撥水性金属・撥水性物質の被覆・撥水性セラミッ
クス・撥水性加工の、何れか１以上で構成した撥水性タ
ービン翼の、外側タービン動翼群１９及び内側タービン
動翼群２０との、摩擦損失を最小として、略直線蛇行的
に噴射して、摩擦損失最少・消費熱量最少・重力パワー
最大で出力を発生し、機械効率を２倍乃至３倍に上昇し
ます。従って後述の全動翼蒸気ガスタービンに近い、燃
焼ガス排気温度を−２７３℃に近付けた、極低温燃焼ガ
スを核に雹や水滴等として凝集して排出する、ＣＯ２等
排気０の全動翼ガスタービンにし、消費燃焼ガス熱量を
０以下も可能とし、熱効率を無限上昇に近付けます。Combustion gas inlet temperature is minimized to bring combustion gas exhaust temperature close to -273.degree. C. to minimize temperature and volume barriers, and compression pressure is approximately twice that of the existing gas turbine, 10M.
Pa is possible and the fuel combustion mass is up to the theoretical air-fuel ratio.
The combustion gas of the lowest temperature obtained by heat-exchange with the fuel combustion of about 4 times that of the existing gas turbine is (2 times the head of the existing gas turbine x the same combustion gas mass x 2 to 3 times the mechanical efficiency) = (existing gas It is an all-blade gas turbine with the same combustion gas mass output (4 to 6 times that of the turbine). In the initial stage of output generation, the cooling of the water-injected combustion gas 10, including the cooling, reduces the volume of the combustion gas to increase the water mass, and the water and the combustion gas 10 whose atmospheric pressure unit gravity power has increased 1700 times, etc. The outer turbine rotor blade group 19 and the inner turbine rotor blade group 20 of a water repellent turbine blade configured by at least one of high temperature, water repellent metal, water repellent substance coating, water repellent ceramics, and water repellent finish. The friction loss is minimized, and the fuel is injected in a substantially linear meandering manner to generate the output with the minimum friction loss, the minimum heat consumption and the maximum gravity power, and the mechanical efficiency is doubled or tripled. Therefore, all moving blades of exhaust gas such as CO2, which is close to a full-blade steam gas turbine described later, whose combustion gas exhaust temperature is close to -273 ° C., and which discharges the cryogenic combustion gas by condensing it into the core as hail, water droplets, etc. By using a gas turbine, the consumed combustion gas heat quantity can be reduced to 0 or less, and the thermal efficiency can approach infinite increase.

【００２３】燃焼ガス１０入口温度を最低にすること
で、全動翼ガスタービン燃焼ガス排気温度を−２７３℃
に近付けて、熱交換して得た燃焼ガス熱量を、供給燃料
全発熱量＋圧縮空気保有熱量−２７３℃以上略全部の熱
回収として、同一燃料量既存ボイラの２倍前後の熱回収
量とします。重力パワーを増大して、小型簡単大出力・
設計容易にして全動翼翼形を可能にし、加熱高温・撥水
性金属・撥水性物質の被覆・撥水性セラミックス・撥水
性加工の、何れか１以上で構成の撥水性外側タービン動
翼群１９及び内側タービン動翼群２０として、水等との
摩擦損失を僅少とし、段落毎環状に一体鋳造８４及び全
自動加工も可能にします。そして鋳造時のタービン翼等
に電気絶縁した電線を配線した、加熱高温手段７９の鋳
込みや、断熱して設けた水噴射手段５６ａの鋳込みを可
能にします。段落毎環状に一体鋳造８４して、外径組立
環状部８５や内径組立環状部８６の接続部で、加熱高温
手段７９や水噴射手段５６ａを接続し、該水噴射手段５
６ａを組立環状接続部付近に設け、品質の良い電気等に
よる加熱高温手段７９や、水噴射手段５６ａを設けた、
撥水性の外側タービン動翼群１９及び内側タービン動翼
群２０とします。By lowering the temperature of the combustion gas 10 at the inlet, the exhaust gas temperature of all moving blade gas turbine combustion gas is -273.degree.
The heat quantity of the combustion gas obtained by heat exchange as the total heat value of the supplied fuel + the heat quantity of the compressed air held at -273 ° C. or more, and the heat recovery quantity of about twice that of the existing boiler. I will. Increases gravitational power to reduce size, size and size
A water-repellent outer turbine blade group 19 composed of any one or more of heating high temperature, water-repellent metal, coating of water-repellent substance, water-repellent ceramics, and water-repellent treatment, which enables easy design and all rotor blades. As the inner turbine rotor blade group 20, friction loss with water etc. is minimized, and it is also possible to perform integral casting 84 and fully automatic processing in an annular shape for each paragraph. Then, it is possible to cast the heating high temperature means 79 and the water jetting means 56a that are provided with heat insulation, in which electrically insulated electric wires are wired to the turbine blade during casting. The paragraphs are integrally cast in an annular shape 84, and the heating high temperature means 79 and the water injection means 56a are connected at the connection portion of the outer diameter assembly annular portion 85 and the inner diameter assembly annular portion 86, and the water injection means 5 is connected.
6a is provided in the vicinity of the assembled annular connecting portion, and high-temperature heating means 79 for high-quality electricity or water injection means 56a is provided.
A water-repellent outer turbine blade group 19 and an inner turbine blade group 20.

【００２４】図２の全動翼蒸気タービンの第１実施例に
は、熱交換して得た同一燃料量既存ボイラの２倍前後の
回収熱量を、超臨界圧力等の水蒸気５として蒸気管６よ
り、蒸気加減弁７を介して最上流に供給します。そして
出力発生の全過程で水噴射水蒸気５を冷却して、水蒸気
容積を縮小して、過熱蒸気速度や気化潜熱の大部分は、
水質量の速度重力パワーにエネルギ変換し、上流の一部
分乃至下流の大部分は、重力パワー大気圧最先端蒸気タ
ービンの１７００倍や、真空部重力パワー１００００倍
以上の、水速度の重力パワーとなり、タービン動翼面積
の一部乃至大部分を、１／１７００や１／１００００に
縮小します。タービン動翼面積の大幅縮小及び、全重力
パワーの大幅増大により、全動翼蒸気タービンを小型簡
単大出力・設計容易にします。In the first embodiment of the all-blade steam turbine shown in FIG. 2, the recovered heat quantity about twice that of the existing boiler having the same fuel quantity obtained by heat exchange is used as steam 5 such as supercritical pressure in the steam pipe 6 Will be supplied to the uppermost stream via the steam control valve 7. Then, the water injection steam 5 is cooled in the whole process of output generation to reduce the steam volume, and most of the superheated steam velocity and latent heat of vaporization are
The energy is converted into velocity gravity power of water mass, and the upstream part to most of the downstream becomes gravity power of water velocity, which is 1700 times as high as the gravity power atmospheric state-of-the-art steam turbine and 10000 times as high as vacuum part gravity power, A part or most of the turbine blade area is reduced to 1/1700 or 1/10000. By greatly reducing the turbine rotor blade area and greatly increasing the total gravity power, it is possible to design a full rotor steam turbine that is small, simple, large in output and easy to design.

【００２５】小型簡単大出力・設計容易にすることで、
凝縮水等を略直線蛇行的に噴射して出力を発生する、全
動翼翼形にすると共に、翼間隔を拡大した翼幅や翼形や
翼角度も、重力パワー増大に合わせた形状にします。そ
して外側タービン動翼群１９及び内側タービン動翼群２
０を、段落毎環状に一体鋳造８４及び全自動加工も可能
にします。そして鋳造時のタービン翼等に電気や燃焼ガ
スや過熱蒸気による、加熱高温手段７９の鋳込みや、断
熱して設けた水噴射手段５６ａの鋳込みを可能にしま
す。段落毎環状に一体鋳造８４して、外径組立環状部８
５や内径組立環状部８６の接続部で、加熱高温手段７９
や水噴射手段５６ａを接続して、品質の良い電気等によ
る加熱高温手段７９や、組立環状接続部付近に水噴射手
段５６ａを設け、断熱した図に無い適宜の冷却手段５５
の水を噴射する、撥水性の外側タービン動翼群１９及び
内側タービン動翼群２０とします。Small, simple, large output, and easy to design,
In addition to a fully moving blade that generates an output by injecting condensed water in a meandering straight line, the blade width, blade shape, and blade angle with expanded blade intervals are also shaped to match the increase in gravity power. The outer turbine blade group 19 and the inner turbine blade group 2
It is also possible to perform one-piece casting 84 in a ring shape for each paragraph and fully automatic processing. Then, it is possible to cast the heating high-temperature means 79 and the water-injection means 56a provided with heat insulation into the turbine blades during casting by electricity, combustion gas, or superheated steam. The outer diameter assembly annular portion 8 is integrally cast 84 in an annular shape for each paragraph.
5 and the connecting portion of the inner diameter assembly annular portion 86, the heating high temperature means 79
Water injection means 56a is connected to heat high temperature means 79 of high quality by electricity or the like, and water injection means 56a is provided in the vicinity of the assembled annular connection portion, and an appropriate cooling means 55 not shown in the figure is insulated.
Water-repellent outer turbine blade group 19 and inner turbine blade group 20 that inject water

【００２６】更に撥水性タービン翼を追加して、加熱高
温・撥水性金属・撥水性物質の被覆・撥水性セラミック
ス・撥水性加工の、何れか１以上で構成の撥水性全動翼
タービン翼と、水等との摩擦損失を僅少として、水蒸気
等を略直線蛇行的に噴射して、摩擦損失最少・消費熱量
最少で出力を発生し、機械効率を２倍乃至３倍に上昇し
て、出力を発生することで、全動翼蒸気タービンの出力
を（既存ガスタービンの５倍落差×２倍回収熱量×２倍
乃至３倍機械効率×真空部１００００倍重力パワー／
〆）＝（既存ガスタービンの２２０倍乃至５３０倍燃焼
ガス熱量出力）にします。全動翼蒸気タービンにしま
す。Further, by adding a water repellent turbine blade, a water repellent full rotor blade turbine blade composed of at least one of heating high temperature, water repellent metal, coating of water repellent substance, water repellent ceramics, and water repellent finish. , The friction loss with water etc. is made small, and the steam etc. are injected in a substantially linear meandering manner to generate the output with the minimum friction loss and the minimum heat consumption, and the mechanical efficiency is doubled to 3 times and output To generate the output of the full-blade steam turbine (5 times the head of the existing gas turbine × 2 times the recovered heat quantity × 2 to 3 times the mechanical efficiency × the vacuum section 10000 times the gravity power /
〆) = (220 to 530 times the combustion gas calorie output of the existing gas turbine). It will be a full-blade steam turbine.

【００２７】図３の全動翼蒸気ガスタービン乃至全動翼
蒸気ガスタービン合体機関の第１実施例に於いて、全動
翼圧縮機の主要部分の、外側圧縮機動翼群１６及び内側
圧縮機動翼群１７の、撥水性金属・撥水性物質の被覆・
撥水性セラミックス・撥水性加工の、何れか１以上で構
成の撥水性水冷却翼８７等を、冷却手段５５により通水
して水冷却し、その水を水噴射手段５６より水噴射して
圧縮空気を直接冷却し、その熱を回収して空気容積を縮
小します。撥水性水冷却翼８７で成る全動翼とすること
で、翼間隔を増大した全動翼翼形として、圧縮空気を略
直線蛇行的に摩擦損失最小で圧縮する、撥水性の外側圧
縮機動翼群１６及び内側圧縮機動翼群１７を、段落毎圧
縮機翼群を環状に一体鋳造８４とします。全自動加工が
可能な環状に一体鋳造８４の組立構造とし、環状鋳造組
立接続部で冷却手段５５の水路を連結して、該組立接続
部付近に水噴射手段５６を設けます。冷却手段５５の水
路を、１以上複数又は段落全部又は段落半分の撥水性水
冷却翼８７を冷却後に、水噴射手段５６より水噴射空気
冷却し、最も効率良く水冷却した低温空気を圧縮しま
す。熱回収した高温補給水と低温圧縮空気により、燃焼
器兼熱交換器４で限りなく燃焼熱交換熱回収して、全動
翼蒸気ガスタービン燃焼ガス入口温度を最低に低下さ
せ、熱回収量を最大に増大し、極低温燃焼ガス排気温度
を−２７３℃に近付けます。In the first embodiment of the all-blade steam gas turbine or the all-blade steam gas turbine combined engine of FIG. 3, the outer compressor blade group 16 and the inner compressor operation of the main part of the all-blade compressor are shown. Coating of blade group 17 with water-repellent metal / water-repellent substance
A water-repellent water cooling blade 87 or the like composed of any one or more of water-repellent ceramics and water-repellent processed is passed by the cooling means 55 to be water-cooled, and the water is jetted from the water jetting means 56 to be compressed. It directly cools the air and recovers its heat to reduce the air volume. A water-repellent outer compressor blade group that compresses compressed air in a substantially linear meandering manner with minimum friction loss by forming a full-rotor blade with a water-repellent water-cooling blade 87 to increase the blade spacing. 16 and the inner compressor rotor blade group 17, the compressor blade group for each paragraph is made into an integrally cast 84. It has an assembly structure of an integral casting 84 in an annular shape that can be fully automated, connects the water passage of the cooling means 55 at the annular casting assembly connection part, and installs the water injection means 56 near the assembly connection part. After cooling the water passage of the cooling means 55 by one or more or all or all or half of the water-repellent water cooling blades 87, the water jetting means 56 cools the water jetting air to compress the most efficiently cooled low temperature air. .. The high temperature make-up water and the low temperature compressed air that have recovered the heat recover the combustion heat exchange heat infinitely in the combustor / heat exchanger 4 to reduce the total moving blade steam gas turbine combustion gas inlet temperature to the minimum and reduce the heat recovery amount. It maximizes and brings the temperature of the cryogenic combustion gas exhaust to near -273 ° C.

【００２８】公害低減・地球温暖化防止が急務であり、
例えば有限の燃料資源を子孫にも残すため、発電用には
安価微粉炭燃料の特定燃焼とし、公知のゴミガス化燃料
やゴミ微細化燃料や、燃えるもの全部の燃焼・熱回収を
可能にし、該燃焼空気を圧縮して再燃焼させ、熱回収し
て電力にします。そこでＣＯ２等燃焼ガス排気を０にす
るため、（全動翼蒸気タービン＋全動翼ガスタービン＝
全動翼蒸気ガスタービン）として使用します。全動翼蒸
気ガスタービンでは、水蒸気５と燃焼ガス１０により出
力を発生増大し、出力発生の過程で水噴射水蒸気を冷却
するため、蒸気速度や気化潜熱の大部分が、重力パワー
大気圧水蒸気の１７００倍の水となり、動翼面積の一部
乃至大部分を１／１７００に縮小して、構造を小型簡単
大出力に出来ます。そして排気前には水蒸気や水を極低
温燃焼ガスにより冷却となり、極低温燃焼ガスを含む微
粉炭燃焼灰を核に、水や水蒸気を凝集して雹や水滴を生
成させて分別し、ＣＯ２等の燃焼ガス排気０を可能に
し、復水器真空まで断熱膨張を可能にします。分別回収
した燃焼灰を含む膨大な雹や水滴は、その一部で水道水
を冷却して冷熱として貯蔵しておき、家庭用や業務用ク
ーラーとして都市部等を丸ごと冷却し、膨大な残りの冷
熱は別途海水を冷却して、海底にＣＯ２等の冷熱を供給
する過程で、酸素等の必要物質を吸引して海中に供給
し、海の生物の生態を微生物まで徹底的に研究して、微
生物や魚介類や海草類や海藻類を繁殖させて、食料の増
産を図ります。There is an urgent need to reduce pollution and prevent global warming,
For example, in order to leave a finite fuel resource to the descendants, a specific combustion of an inexpensive pulverized coal fuel is used for power generation, and it is possible to burn and recover heat of all known waste gasification fuels, waste atomization fuels, and all combustible materials. Combustion air is compressed and recombusted to recover heat and generate electricity. Therefore, in order to reduce the exhaust gas of combustion gas such as CO2 to 0 (total moving blade steam turbine + total moving blade gas turbine =
Full-blade steam gas turbine). In an all-blade steam gas turbine, an output is increased by the steam 5 and the combustion gas 10 and the water-injected steam is cooled in the process of generating the output. Therefore, most of the steam velocity and latent heat of vaporization are generated by gravity power atmospheric pressure steam. It becomes 1700 times as much water, and a part or most of the blade area can be reduced to 1/1700, and the structure can be made compact and simple with a large output. Before the exhaust, steam and water are cooled by the cryogenic combustion gas, and pulverized coal combustion ash containing the cryogenic combustion gas is used as a core to agglomerate water and steam to generate hail and water droplets for separation, such as CO2. It enables zero combustion gas exhaust and enables adiabatic expansion up to the condenser vacuum. A huge amount of hail and water droplets containing combustion ash that has been separated and collected is stored as cold heat by cooling tap water in a part of it, and it cools the entire city area as a home or commercial cooler, and the huge remaining In the process of cooling cold seawater separately, in the process of supplying cold heat such as CO2 to the seabed, necessary substances such as oxygen are sucked and supplied into the sea, and the ecology of sea life is thoroughly studied up to microorganisms, We aim to increase the production of food by breeding microorganisms, seafood, seaweeds, and seaweeds.

【００２９】例えば水蒸気５を水噴射冷却して水を増大
し、水蒸気気化潜熱を含む質量速度の一部乃至大部分
を、大気圧重力パワー１７００倍・真空部重力パワー１
００００倍以上の、水重力パワーにエネルギ変換しま
す。そして例えば燃焼ガス質量発電量を（既存ガスター
ビンの２倍落差×石炭灰等２倍質量×２倍乃至３倍機械
効率）＝（既存ガスタービンの８倍乃至１２倍燃焼ガス
質量発電量）に増大して、資源の有効利用を可能にしま
す。そして（燃焼ガス質量発電量＋燃焼ガス熱量発電
量）＝（８倍乃至１２倍＋２２０倍乃至５３０倍）＝
（２２８倍乃至５４２倍全動翼蒸気ガスタービン発電
量）にします。出力発生の後期には、極低温燃焼ガスを
核に水や水蒸気を凝集して燃焼ガス０とし、雹や水滴と
して復水器真空まで膨張させ、気化潜熱の略全部に近い
水の重力パワーが、終段では最先端技術の１００００倍
に近付くため、小型簡単な設計が可能となり、非常に大
きな全重力パワーにより、考えられない程大量の発電量
にします。For example, the steam 5 is water-jet-cooled to increase the amount of water, and a part or most of the mass velocity including the steam vaporization latent heat is converted into atmospheric pressure gravity power 1700 times and vacuum portion gravity power 1
Energy is converted into water gravity power of 0000 times or more. Then, for example, the combustion gas mass power generation amount is set to (double head of existing gas turbine x double mass of coal ash etc. x 2 to 3 times mechanical efficiency) = (8 to 12 times combustion gas mass power generation amount of existing gas turbine) Increase and enable effective use of resources. And (combustion gas mass power generation + combustion gas calorific power generation) = (8 to 12 times + 220 to 530 times) =
(228 to 542 times full rotor steam gas turbine power generation). In the latter stage of the output generation, water and steam are condensed into the combustion gas 0 with the cryogenic combustion gas as the nucleus, and expanded to the condenser vacuum as hail and water droplets. In the final stage, it approaches 10,000 times the state-of-the-art technology, so a small and simple design is possible, and due to the extremely large total gravity power, it produces an unimaginable amount of power.

【００３０】又極低温燃焼ガスを含む雹や水滴は、環境
に排出する過程で、有効利用するのが好ましい。そこで
最も効率良く環境に排出する全動翼蒸気ガスタービンと
し、復水を最も多く効率良く回収使用のため、全動翼蒸
気タービンを併用して、同一燃料燃焼ガス熱量出力を、
既存ガスタービンの２２０倍乃至５３０倍出力の大部分
とし、発電量に変換して復水は従来どうりに循環使用し
ます。そして最適量の水蒸気と燃焼ガス全部により、全
動翼蒸気ガスタービンを運転して、極低温燃焼ガスを含
む雹や水滴を最低温度で排出し、水道水等を冷却貯蔵し
ておき、家庭用や業務用クーラーとして都市部等を丸ご
と冷却したり、膨大な残りの冷熱は別途海水を冷却し
て、海底にＣＯ２等の冷熱を供給する過程で、酸素等の
必要物質を吸引して海中に供給し、海の生物の生態を微
生物まで徹底的に研究して、微生物や魚介類や海草類や
海藻類を繁殖させて、食料の増産を図ります。そしてＣ
Ｏ２等燃焼ガス排気０を可能にします。Further, it is preferable to effectively use the hail and water droplets containing the cryogenic combustion gas in the process of discharging to the environment. Therefore, a full-blade steam gas turbine that most efficiently discharges to the environment is used, and in order to recover and use most of the condensate most efficiently, a full-blade steam turbine is also used to output the same fuel combustion gas calorific value.
Most of the output is 220 to 530 times that of the existing gas turbine, and the condensate is converted to the amount of power generation and recycled as before. Then, with the optimum amount of steam and combustion gas, operate the full-blade steam gas turbine to discharge hail and water droplets containing cryogenic combustion gas at the lowest temperature, cool and store tap water, etc. for household use. As a commercial cooler, it cools an entire city, etc., or the enormous amount of remaining cold heat is cooled separately from seawater, and in the process of supplying cold heat such as CO2 to the seabed, it sucks in necessary substances such as oxygen and puts them in the sea. We will supply and thoroughly study the ecology of marine organisms up to microorganisms, breed microorganisms, seafood, seaweeds, and seaweeds to increase food production. And C
Enables zero combustion gas exhaust such as O2.

【００３１】用途に合わせて各種燃料を燃焼して、回転
力を利用する自動車等の各種陸上輸送機器や、陸海空の
各種機器の用途には各種燃料を燃焼して、燃焼器兼熱交
換器４で限りなく燃焼熱交換して熱回収し、燃焼ガス排
気温度を−２７３℃に近付け、熱回収量を既存ボイラの
２倍前後の回収熱量に増大し、圧縮空気圧力を既存ガス
タービンの２倍の、１０ＭＰａ以上を可能にして、理論
空燃比まで、既存ガスタービンの４倍前後の燃料を燃焼
可能にします。熱交換して得た既存ボイラの２倍前後の
燃焼ガス熱量を、超臨界圧力等の水蒸気５として、全動
翼蒸気ガスタービンの最上流に供給し、中流最適段に燃
焼ガス質量出力の燃焼ガス１０を供給します。そして
（既存ガスタービンの５倍落差×２倍熱量×２乃至３倍
機械効率×１７００倍重力パワー／〆）＋（既存ガスタ
ービンの２倍落差×２乃至３倍機械効率）＝（既存ガス
タービンの１２０倍乃至１３０倍燃焼ガス熱量出力）＋
（４倍乃至６倍燃焼ガス質量出力）＝（１２４倍乃至１
３６倍全動翼蒸気ガスタービン出力）とします。排気前
には水蒸気や水を極低温燃焼ガスにより冷却となりま
す。そしてＣＯ２等の極低温燃焼ガスを核に、水や水蒸
気を凝集して、雹や水滴を生成させて、燃焼ガスの１０
０倍質量等の水と共に分別回収し、該水には化学物質等
の物質を混入して、ＣＯ２等の公害ガスを水に合成溶解
混合して排出し、ＣＯ２等の有害燃焼ガス排気０を可能
にします。Combustion of various fuels according to the application, combustion of various fuels for use in various types of land transportation equipment such as automobiles and various equipment of land, sea and air that utilize rotational force, and combustion and heat exchanger 4 Endlessly recovering heat by exchanging combustion heat, making the exhaust gas exhaust temperature close to -273 ° C, increasing the heat recovery amount to about twice the heat recovery amount of the existing boiler, and doubling the compressed air pressure of the existing gas turbine. It is possible to burn 10MPa or more and up to 4 times the fuel of the existing gas turbine up to the theoretical air-fuel ratio. About twice the combustion gas calorific value of the existing boiler obtained by heat exchange is supplied as the steam 5 of supercritical pressure to the uppermost stream of the full-blade steam gas turbine, and the combustion gas mass output is combusted in the middle-stream optimal stage. Supply gas 10. And (5x head of existing gas turbine x 2x amount of heat x 2 to 3 times mechanical efficiency x 1700 times gravity power / 〆) + (2x head of existing gas turbine x 2 to 3 times mechanical efficiency) = (existing gas turbine 120 to 130 times the heat output of combustion gas) +
(4 to 6 times combustion gas mass output) = (124 to 1 times
36 times all moving blade steam gas turbine output). Before exhausting, steam and water are cooled by cryogenic combustion gas. Then, water and water vapor are condensed by using a cryogenic combustion gas such as CO2 as a nucleus to generate hail and water droplets.
It is separated and collected together with water of 0 times mass and the like, substances such as chemical substances are mixed in the water, and pollution gas such as CO2 is synthetically dissolved and mixed in water and discharged, and exhaust gas 0 of harmful combustion gas such as CO2 is discharged. Enable

【００３２】自動車等全出力で回転力発生の小型全動翼
蒸気ガスタービンでも、水蒸気５と燃焼ガス１０により
出力を発生増大するため、出力発生の前中期過程で水噴
射水蒸気を冷却し、中後期過程で燃焼ガス入口前の水噴
射燃焼ガス冷却を含めた、最低温度の燃焼ガスを最適段
に供給して、出力を発生します。水噴射冷却により水蒸
気容積は縮小して、排気前には気化潜熱の大部分が、水
質量の速度パワーにエネルギ変換して、膨大な出力とな
ります。上流部分の一部乃至下流の大部分は、重力パワ
ー大気圧１７００倍の水質量速度パワーとなり、撥水性
タービン動翼面積の一部乃至大部分を、１／１７００等
に縮小を可能にします。撥水性タービン動翼面積の大幅
縮小及び、全重力パワーの大幅増大により、全動翼蒸気
ガスタービンを小型簡単大出力・設計容易にします。小
型簡単大出力・設計容易にすることで、水蒸気や水や燃
焼ガス等を略直線蛇行的に噴射して出力を発生する、全
動翼翼形にすると共に、翼間隔を拡大した翼幅や翼形や
翼角度も、重力パワー増大に合わせた形状にします。そ
して撥水性の、外側タービン動翼群１９及び内側タービ
ン動翼群２０を、加熱高温・撥水性金属・撥水性物質の
被覆・撥水性セラミックス・撥水性加工の、何れか１以
上で構成の撥水性全動翼タービン翼と、水等との摩擦損
失を最小にして、略直線蛇行的に噴射して、摩擦損失最
少・消費熱量最少で出力を発生し、機械効率を２倍乃至
３倍に上昇します。Even in a small-sized full-blade steam gas turbine that produces a rotational force at full power output, such as an automobile, the power output is increased by the steam 5 and the combustion gas 10. In the latter stage process, the lowest temperature combustion gas including the water injection combustion gas cooling before the combustion gas inlet is supplied to the optimum stage to generate the output. The volume of water vapor is reduced by water injection cooling, and most of the latent heat of vaporization is converted into velocity power of water mass before exhaustion, resulting in a huge output. Part of the upstream part or most of the downstream part has a water mass velocity power of 1700 times the gravity power atmospheric pressure, which makes it possible to reduce part or most of the water repellent turbine blade area to 1/1700. The water-repellent turbine blade area is greatly reduced and the total gravity power is greatly increased, making the full-blade steam gas turbine small, simple, large output, and easy to design. Compact, simple, large output ・ By making design easy, steam, water, combustion gas, etc. are injected in a substantially linear meandering manner to generate output. The shape and wing angle are also adjusted to match the increase in gravity power. The water-repellent outer turbine blade group 19 and the inner turbine blade group 20 are made of any one or more of high-temperature heating, water-repellent metal, water-repellent substance coating, water-repellent ceramics, and water-repellent processing. Minimize friction loss between water-based rotor blades and water, etc., and inject almost linearly in a meandering manner to generate output with minimum friction loss and minimum heat consumption, and double or triple mechanical efficiency Rise

【００３３】図４の全動翼蒸気ガスタービン乃至全動翼
蒸気ガスタービン合体機関の第２実施例は、ジェット機
や飛行船舶や船舶等を噴射推進させる過程を、水蒸気５
の一部と燃焼ガス１０の全部により、全動翼蒸気ガスタ
ービンを駆動して全動翼圧縮機を駆動し、水蒸気５の大
部分を、公知技術を含む霧吹きの原理９１を利用してバ
イパス噴射し、夫々前方の空気を吸引して噴射推進させ
るものです。全動翼圧縮機の主要部分の、外側圧縮機動
翼群１６及び内側圧縮機動翼群１７の撥水性水冷却翼８
７等を、冷却手段５５により通水して水冷却し、その水
を水噴射手段５６より水噴射して圧縮空気を直接冷却
し、その熱を回収利用して空気容積を縮小します。全動
翼とすることで翼間隔を増大した全動翼翼形として、圧
縮空気を略直線蛇行的に圧縮する、撥水性水冷却翼８７
で成る、外側圧縮機動翼群１６及び内側圧縮機動翼群１
７を、段落毎圧縮機翼を環状に一体鋳造８４とします。
全自動加工が可能な環状に一体鋳造８４の組立構造と
し、環状鋳造組立接続部で冷却手段５５の水路を連結し
て、該組立環状接続部付近に水噴射手段５６を設けま
す。冷却手段５５の水路を撥水性水冷却翼８７を冷却後
に、水噴射手段５６より水噴射空気冷却し、最も効率良
く水冷却した低温空気を圧縮します。熱回収した高温補
給水と低温圧縮空気により、燃焼器兼熱交換器４で限り
なく燃焼熱交換熱回収して、全動翼蒸気ガスタービン燃
焼ガス入口温度を最低に低下させ、同一燃料量の回収燃
焼ガス熱量を、既存ボイラの２倍前後の熱回収量にしま
す。The second embodiment of the all-moving-blade steam gas turbine or the all-moving-blade steam gas turbine combined engine shown in FIG. 4 is that the process of injecting and propelling a jet aircraft, a flying ship, a ship, etc.
Of the combustion gas 10 and all of the combustion gas 10 to drive the full-blade steam gas turbine to drive the full-blade compressor, and most of the water vapor 5 is bypassed by utilizing the atomization principle 91 including a known technique. It injects and sucks the air in front of each to propel it. The water-repellent water cooling blades 8 of the outer compressor blade group 16 and the inner compressor blade group 17 of the main part of the whole rotor compressor.
The water is cooled by passing water through the cooling means 55 through the cooling means 55, and water is jetted by the water jetting means 56 to directly cool the compressed air, and the heat is recovered to reduce the air volume. A water repellent water cooling blade 87 that compresses compressed air in a substantially linear meandering manner as a full moving blade airfoil whose blade spacing is increased by using all moving blades.
An outer compressor blade group 16 and an inner compressor blade group 1
7, the compressor blade is made into a ring-shaped integral casting 84 for each paragraph.
The assembly structure is an integrally cast 84 ring that can be fully automatically processed. The water channel of the cooling means 55 is connected at the ring casting assembly connection part, and the water injection means 56 is provided near the assembly ring connection part. After cooling the water repellent water cooling vanes 87 in the water passages of the cooling means 55, the water jetting means 56 cools the water jetting air to compress the water-cooled low temperature air most efficiently. With the high temperature makeup water and low temperature compressed air that have recovered heat, combustion heat exchange heat is recovered infinitely in the combustor and heat exchanger 4 to reduce the total moving blade steam gas turbine combustion gas inlet temperature to the minimum, The recovered combustion gas heat quantity is set to about twice that of the existing boiler.

【００３４】公害低減・地球温暖化防止が急務でありま
す。そこでＣＯ２等燃焼ガス排気を０にするため、噴射
推進を含む全動翼蒸気ガスタービンでは、例えば５／２
４の水蒸気５の一部と、燃焼ガス１０の全部により、全
動翼圧縮機を含む全動翼蒸気ガスタービンを駆動して排
気し、内側軸装置の中空部や本体外周部の空気を吸引し
て噴射推進します。１９／２４前後の水蒸気５により、
公知技術を含む霧吹きの原理９１ａを利用して蒸気管６
より水蒸気５を噴射して、前方の空気を多段に吸引し
て、最適速度で噴射して推進する特殊装置９２ａによ
り、用途に合わせた噴射速度で噴射推進します。燃焼ガ
ス排気温度を最低に低下させ、熱回収量を増大し、水蒸
気５と燃焼ガス１０により、全動翼蒸気ガスタービンの
出力を発生するため、排気前には水蒸気や水を極低温燃
焼ガスにより冷却となり、極低温燃焼ガスを核に凝集す
る、水蒸気や水等の凝集を容易にします。そして極低温
燃焼ガスを核に水や水蒸気を凝集して、自然現象と同様
に雹や水滴を生成して噴射推進し、海水等を冷却してＣ
Ｏ２等の燃焼ガス排気０を可能にします。There is an urgent need to reduce pollution and prevent global warming. Therefore, in order to reduce the exhaust gas of combustion gas such as CO2 to 0, in a full-blade steam gas turbine including injection propulsion, for example, 5/2
Part of the water vapor 5 of 4 and all of the combustion gas 10 drive and exhaust the full-blade steam gas turbine including the full-blade compressor, and suck air in the hollow part of the inner shaft device and the outer peripheral part of the main body. And promote the injection. By steam 5 around 19/24,
The steam pipe 6 utilizing the spraying principle 91a including a known technique.
A special device 92a that injects more water vapor 5 and sucks the air in the front in multiple stages and injects at the optimum speed to propel it at an injection speed suitable for the application. The combustion gas exhaust temperature is lowered to the minimum, the amount of heat recovery is increased, and the steam 5 and the combustion gas 10 generate the output of the full-blade steam gas turbine. It cools down and makes the cryogenic combustion gas agglomerate in the nucleus, facilitating the agglomeration of water vapor and water. Then, water and water vapor are condensed by using the cryogenic combustion gas as a nucleus to generate hail and water droplets as in the case of a natural phenomenon to inject and propel them to cool seawater etc.
It enables zero combustion gas exhaust such as O2.

【００３５】例えば水蒸気速度を水噴射冷却して水質量
を増大し、水蒸気の一部乃至大部分を大気圧重力パワー
１７００倍の水を増大します。即ち燃焼器兼熱交換器４
で限りなく燃焼熱交換して熱回収し、燃焼ガス排気温度
を−２７３℃に近付け、温度と容積の障害を最低にし、
圧縮空気圧力を既存ガスタービンの２倍の、１０ＭＰａ
以上にして理論空燃比まで、既存ガスタービンの４倍前
後の燃料を燃焼可能にします。該熱交換して得た従来４
倍燃料全発熱量＋圧縮した空気の−２７３℃以上略全熱
量の内、同一燃料量既存ボイラの２倍前後の回収熱量
を、超臨界圧力等の水蒸気５としてその一部を、全動翼
蒸気ガスタービンの最上流に供給し、中流最適段に最低
温度の燃焼ガス１０全部を供給します。そして（既存ガ
スタービンの１２０倍乃至１３０倍燃焼ガス熱量出力＋
４倍乃至６倍燃焼ガス質量出力）＝（既存ガスタービン
の１２４倍乃至１３６倍バイパス噴射を含む全動翼蒸気
ガスタービン出力）とします。全動翼蒸気ガスタービン
駆動噴射出力は重力パワーで増大し、公知技術を含む霧
吹きの原理９１を利用してバイパス使用する、例えば１
９／２４出力の水蒸気５は、その水蒸気速度を直接空気
の速度にエネルギ変換して、更に効率良く大量の空気を
含めて噴射推進します。For example, the water mass is increased by water jet cooling of the water vapor velocity, and a part or most of the water vapor is increased by water having an atmospheric pressure gravity power of 1,700 times. That is, combustor and heat exchanger 4
With infinite combustion heat exchange to recover heat, exhaust gas exhaust temperature close to -273 ℃, to minimize temperature and volume obstacles,
Compressed air pressure is twice the existing gas turbine, 10 MPa
In this way, it is possible to burn up to about 4 times the fuel of existing gas turbines up to the theoretical air-fuel ratio. Conventional 4 obtained by the heat exchange
Double fuel total calorific value + Compressed air at -273 ° C or higher Nearly the total calorific value of the same fuel amount, about twice as much as the recovered heat amount of the existing boiler, a part of the recovered heat amount as steam 5 at supercritical pressure It supplies the uppermost stream of the steam gas turbine and supplies all 10 of the lowest temperature combustion gas to the optimum middle stage. And (120 to 130 times the combustion gas calorie output of the existing gas turbine +
4 to 6 times combustion gas mass output) = (124 to 136 times the existing gas turbine full blade steam gas turbine output including bypass injection). Full-blade steam gas turbine drive injection power increases with gravity power and is bypassed utilizing atomization principles 91 including known techniques, eg 1
9/24 output water vapor 5 directly converts the water vapor velocity into the velocity of the air and injects and propels more efficiently a large amount of air.

【００３６】図５の全動翼蒸気ガスタービン合体機関乃
至全動翼蒸気タービンの第２実施例は、燃焼ガス１０全
部を公知技術を含む霧吹きの原理９１ｂを利用して、特
殊装置９２ｂよりバイパス噴射して、前方の空気を多段
に吸引して噴射推進し、水蒸気５の一部を、公知技術を
含む霧吹きの原理９１ａを利用して、特殊装置９２ａよ
り同様にバイパス噴射推進し、水蒸気５の一部により、
全動翼圧縮機を含む全動翼蒸気タービンを駆動して噴射
推進する、ジェット機や噴射推進飛行船舶や宇宙往還親
飛行機等とするものです。全動翼圧縮機の主要部分の、
外側圧縮機動翼群１６及び内側圧縮機動翼群１７の撥水
性水冷却翼８７等を、冷却手段５５により通水して水冷
却し、その水を水噴射手段５６より水噴射して圧縮空気
を直接冷却し、その熱を回収して空気容積を縮小しま
す。全動翼とすることで翼間隔を増大した全動翼翼形と
して、圧縮空気を略直線蛇行的に圧縮する、撥水性水冷
却翼８７で成る、外側圧縮機動翼群１６及び内側圧縮機
動翼群１７を、段落毎圧縮機翼を環状に一体鋳造８４と
します。全自動加工が可能な環状に一体鋳造８４の組立
構造とし、環状鋳造組立接続部で冷却手段５５の水路を
連結して、該組立環状接続部付近に水噴射手段５６を設
けます。冷却手段５５の水路を撥水性水冷却翼８７を冷
却後に、水噴射手段５６より水噴射直接接触空気冷却
し、最も効率良く水冷却して低温空気を圧縮します。熱
回収した高温補給水と低温圧縮空気により、燃焼器兼熱
交換器４で限りなく燃焼熱交換熱回収して、全動翼蒸気
タービンの燃焼ガス取出口８８の、燃焼ガス温度を最低
に低下させます。The second embodiment of the all-blade steam gas turbine combined engine or the all-blade steam turbine shown in FIG. 5 bypasses the combustion gas 10 from the special device 92b by utilizing the atomization principle 91b including a known technique. By injecting, the air in front is sucked in multiple stages to inject and propel, and a part of the steam 5 is similarly bypass-injected and propelled by the special device 92a by utilizing the mist-blowing principle 91a including a known technique. By part of
It is a jet machine, a jet propulsion flying ship, a space shuttle parent plane, etc. that drives and propels the full-blade steam turbine including the full-blade compressor. Of the main part of the full-blade compressor,
The water repellent water cooling blades 87 of the outer compressor blade group 16 and the inner compressor blade group 17 are water-cooled by passing water by the cooling means 55, and the water is jetted from the water jetting means 56 to generate compressed air. It directly cools and recovers its heat to reduce the air volume. An outer compressor blade group 16 and an inner compressor blade group, which are water-repellent water cooling blades 87, which compress compressed air in a substantially linear meandering manner, as a total rotor blade airfoil whose blade spacing is increased by using all rotor blades. No. 17 is a unitary casting 84 of the compressor blades in an annular shape for each paragraph. The assembly structure is an integrally cast 84 ring that can be fully automatically processed. The water channel of the cooling means 55 is connected at the ring casting assembly connection part, and the water injection means 56 is provided near the assembly ring connection part. After cooling the water repellent water cooling vanes 87 in the water passage of the cooling means 55, the water jetting means 56 performs water jet direct contact air cooling to cool the water most efficiently and compress the low temperature air. The recovered high-temperature makeup water and the low-temperature compressed air are used to infinitely recover the combustion heat exchange heat in the combustor / heat exchanger 4 to lower the combustion gas temperature at the combustion gas outlet 88 of the all-blade steam turbine to the minimum. I will let you.

【００３７】全動翼蒸気タービン等の動圧や反動で駆動
する回転機関は、超臨界圧力過熱蒸気等と、大きな落差
を設定しても合理的設計を可能にし、動圧出力の増大を
容易にするため、単位重力パワーの増大を最重要としま
す。即ち大気圧単位重力パワーを１７００倍に増大し
て、該動翼面積を１／１７００等に縮小が容易な水蒸気
５の一部で、全動翼蒸気タービンを駆動し、燃焼ガス１
０全部及び残りの水蒸気５を、動圧の逆で吸引の霧吹き
の原理を利用して、バイパス噴射して吸引噴射推進しま
す。例えば水蒸気５の一部により、全動翼圧縮機を含む
全動翼蒸気タービンを駆動し、排気の過程で公知技術を
含む霧吹きの原理９１を利用して、内側軸装置の中空部
や本体外周部の空気を吸引して噴射推進します。残りの
水蒸気５と燃焼ガス１０全部を夫々バイパス噴射によ
り、公知技術を含む霧吹きの原理９１ａ・９１ｂを利用
して、前方の空気を夫々多段に吸引して夫々の速度を直
接空気の速度にエネルギ変換し、減速して噴射質量を増
大することで、最適速度で最も効率良く噴射推進する、
特殊装置９２ａや特殊装置９２ｂとして、用途に合わせ
た噴射速度で最も効率良く噴射推進します。A rotary engine driven by dynamic pressure or reaction of a full-blade steam turbine or the like enables rational design even if a large head is set, such as supercritical pressure superheated steam, and facilitates increase of dynamic pressure output. Therefore, increasing the unit gravity power is the most important factor. That is, the atmospheric power unit gravity power is increased 1700 times and the moving blade area is easily reduced to 1/1700 or the like.
By using the principle of suction mist blowing with the reverse of dynamic pressure, all of the steam 0 and the remaining water vapor 5 are bypass-injected and suction-injected. For example, a part of the water vapor 5 drives a full-blade steam turbine including a full-blade compressor, and in the process of exhausting, utilizing the mist-blowing principle 91 including a known technique, the hollow part of the inner shaft device and the outer periphery of the main body are used. Part of the air is sucked in and propelled. By using the mist-blowing principles 91a and 91b including a known technique, the remaining water vapor 5 and all of the combustion gas 10 are bypass-injected, respectively, and the front air is sucked in multiple stages and the respective velocities are directly converted into the air velocities. By converting, decelerating and increasing the injection mass, the most efficient injection propulsion at the optimum speed,
As the special device 92a and the special device 92b, it will most efficiently inject and propel the injection speed according to the application.

【００３８】燃焼器兼熱交換器４で限りなく燃焼熱交換
して熱回収し、燃焼ガス取出口８８の、燃焼ガス温度を
最低に低下させて、水蒸気回収量を最大に増大し、熱交
換して得た、従来４倍燃料全発熱量＋圧縮した空気の−
２７３℃以上略全熱量の熱回収とし、（燃焼ガス熱量出
力＋燃焼ガス質量出力＝既存ガスタービンの１２４倍乃
至１３６倍出力）にします。そして同一燃料量既存ボイ
ラの２倍前後の回収熱量の燃焼ガス熱量出力を、超臨界
圧力等の水蒸気５として、例えば一部を全動翼蒸気ター
ビンの最上流に供給し、出力発生の全過程で水噴射水蒸
気を冷却し、水蒸気速度や気化潜熱の大部分を、大気圧
１７００倍重力パワー水質量速度にエネルギ変換して、
最も効率良く膨大な回転出力及び噴射出力を発生させま
す。そして霧吹きの原理を利用して、残りの水蒸気５と
燃焼ガス１０を、夫々バイパス噴射して更に効率良く出
力を発生するため、排気の過程で水蒸気や水を極低温燃
焼ガスにより冷却となり、極低温燃焼ガスを核に凝集す
る、水蒸気や水の凝集を容易にします。そして極低温燃
焼ガスを核に水や水蒸気を凝集して、雹や水滴を生成し
て、ＣＯ２等の燃焼ガス排気０を可能にします。The combustor / heat exchanger 4 exchanges heat by infinitely exchanging heat to recover heat, lowers the temperature of the combustion gas at the combustion gas outlet 88 to the minimum, and increases the amount of steam recovery to the maximum, thereby exchanging heat. 4 times the conventional fuel total calorific value + compressed air
The heat recovery is about 273 ℃ or more, and the total heat output is (combustion gas heat output + combustion gas mass output = 124 to 136 times output of existing gas turbine). Then, the combustion gas calorific value output of the recovered calorific value of about twice that of the existing boiler with the same fuel amount is supplied as the steam 5 of the supercritical pressure or the like, for example, a part thereof is supplied to the most upstream of the full-blade steam turbine, and the whole process of the output generation is performed. To cool the water-injected steam, convert most of the steam velocity and latent heat of vaporization into 1700 times atmospheric pressure gravity power water mass velocity,
The most efficient and enormous rotation output and injection output are generated. Then, by utilizing the principle of atomization, the remaining steam 5 and the combustion gas 10 are bypass-injected respectively to generate the output more efficiently, so that the steam and water are cooled by the cryogenic combustion gas during the exhaust process, Facilitates the agglomeration of water vapor and water, which agglomerates low-temperature combustion gases into the nucleus. Then, water and water vapor are condensed by using the cryogenic combustion gas as a nucleus to generate hail and water droplets, which enables zero exhaust of combustion gas such as CO2.

【００３９】図６の全動翼蒸気ガスタービン合体機関乃
至全動翼蒸気タービンの第３実施例は、燃焼ガス１０全
部及び水蒸気５の一部を、夫々１段以上バイパス噴射し
て、公知技術を含む霧吹きの原理９１ｃ・９１ｄを利用
して前方の水を多段に吸引して、１以上複数の水噴射装
置９３ａ・９３ｂにより噴射推進する、船舶等の各種水
上移動機器として使用し、全動翼蒸気タービンの排気噴
射推力により、浮上推進するものが第３実施例です。全
動翼圧縮機の主要部分の撥水性水冷却翼８７で構成の、
外側圧縮機動翼群１６及び内側圧縮機動翼群１７の、冷
却手段５５の水路を撥水性水冷却翼８７を冷却後に、水
噴射手段５６より水噴射して直接空気を冷却し、その熱
を回収して空気容積を縮小し、最も効率良く水冷却した
低温空気を圧縮します。熱回収した高温補給水と低温圧
縮空気により、燃焼器兼熱交換器４で限りなく燃焼熱交
換熱回収して、燃焼ガス取出口８８の温度を最低等に低
下させます。全動翼とすることで翼間隔を増大した全動
翼翼形として、圧縮空気を略直線蛇行的に圧縮する、撥
水性水冷却翼８７で成る、外側圧縮機動翼群１６及び内
側圧縮機動翼群１７を、段落毎に環状に一体鋳造８４し
ます。全自動加工が可能な環状に一体鋳造８４の組立構
造とし、環状鋳造組立接続部で冷却手段５５の水路を連
結して、該組立環状接続部付近に水噴射手段５６を設け
ます。In the third embodiment of the all-blade steam gas turbine combined engine or the all-blade steam turbine shown in FIG. 6, all the combustion gas 10 and a part of the steam 5 are bypass-injected by one or more stages, respectively, to obtain a known technique. Using the principle of spraying 91c and 91d including water, the front water is sucked in multiple stages and is propelled by one or more water jetting devices 93a and 93b. In the third embodiment, the levitation propulsion is performed by the exhaust injection thrust of the blade steam turbine. Of the water repellent water cooling blade 87 of the main part of the full-blade compressor,
After cooling the water repellent water cooling blades 87 in the water passages of the cooling means 55 of the outer compressor blade group 16 and the inner compressor blade group 17, water is jetted from the water jetting means 56 to directly cool the air and recover the heat. To reduce the air volume and most efficiently compress the water-cooled cold air. With the high temperature makeup water and low temperature compressed air that have recovered heat, the combustion heat exchange heat is recovered infinitely in the combustor and heat exchanger 4, and the temperature of the combustion gas outlet 88 is lowered to the minimum. The outer compressor blade group 16 and the inner compressor blade group, which are water-repellent water cooling blades 87, which compress compressed air in a substantially linear meandering manner, are formed as full-rotor blades whose blade spacing is increased by using all rotor blades. 17 is cast integrally in a ring for each paragraph 84. The assembly structure is an integrally cast 84 ring that can be fully automatically processed. The water channel of the cooling means 55 is connected at the ring casting assembly connection part, and the water injection means 56 is provided near the assembly ring connection part.

【００４０】動圧と反動で回転力を発生するタービンで
は、単位重力パワーの増大が最重要のため、全動翼蒸気
タービンを使用します。燃焼器兼熱交換器４で限りなく
燃焼熱交換して熱回収し、圧縮空気圧力を既存ガスター
ビンの２倍の、１０ＭＰａ以上を可能にして、圧縮空気
量を同じで理論空燃比まで、既存ガスタービンの４倍前
後の燃料を燃焼可能にします。該熱交換して得た、従来
４倍燃料全発熱量＋圧縮した空気の−２７３℃以上略全
熱量の熱回収とし、（燃焼ガス熱量出力＋燃焼ガス質量
出力＝既存ガスタービンの１２４倍乃至１３６倍出力）
にします。そして水蒸気５の一部により、全動翼圧縮機
を含む全動翼蒸気タービンを駆動し、排気の過程で霧吹
きの原理９１を利用して、逆止弁付の内側軸装置の中空
部や本体外周部の、前方の空気を吸引して噴射し、船体
を浮上させて噴射推進させます。残りの水蒸気５と燃焼
ガス１０全部を、夫々霧吹きの原理９１ｃ・９１ｄを利
用して、夫々の水噴射装置９３ａ・９３ｂより、夫々１
以上複数のバイパス噴射して、夫々前方の水を多段に吸
引して、夫々の速度を直接水の速度質量にエネルギ変換
して最適減速し、更に効率良く大量の水を含めて噴射推
進します。For a turbine that generates rotational force due to dynamic pressure and reaction, an all-blade steam turbine is used because increasing the unit gravity power is the most important factor. Combustor and heat exchanger 4 exchanges combustion heat as much as possible to recover heat, enabling compressed air pressure to be 10 MPa or more, which is twice the pressure of existing gas turbines, and the amount of compressed air remains the same, up to the theoretical air-fuel ratio. It enables combustion of about 4 times the fuel of a gas turbine. Conventionally, the total heat generation amount of the fuel obtained by the heat exchange is +4 times, and the heat recovery of the compressed air is approximately −273 ° C. or more and substantially the total heat amount of (combustion gas calorific value output + combustion gas mass output = 124 times the existing gas turbine or 136 times output)
I will. Then, a part of the water vapor 5 drives the full-blade steam turbine including the full-blade compressor, and the principle 91 of atomization is used in the process of exhausting to make use of the hollow part and the main body of the inner shaft device with the check valve. The air in front of the outer periphery is sucked and jetted, and the hull is levitated and propelled. The remaining water vapor 5 and all of the combustion gas 10 are respectively discharged from the respective water injection devices 93a and 93b using the spraying principles 91c and 91d.
By performing multiple bypass injections, the water in front of each is sucked in multiple stages, the respective speeds are directly converted into the velocity mass of the water energy for optimal deceleration, and more efficient injection and propelling of a large amount of water is performed. .

【００４１】そして同一燃料量既存ボイラの２倍前後の
回収熱量の燃焼ガス熱量出力を、超臨界圧力等の水蒸気
５として、その一部を全動翼蒸気タービンの最上流に供
給し、出力発生の全過程で水噴射水蒸気を冷却し、水蒸
気速度や気化潜熱の大部分を、大気圧１７００倍重力パ
ワー水質量速度にエネルギ変換して、最も効率良く回転
出力及び噴射出力を発生させ、噴射出力は浮上出力とし
ます。そしてバイパス使用する残りの過熱蒸気５を噴射
して海水等吸引して、最適速度で噴射推進する、霧吹き
の原理９１ｃを利用した水噴射装置９３ａや、燃焼ガス
１０を噴射して前方の水を吸引し、噴射して海水等を最
適速度で噴射推進する水噴射装置９３ｂとして、用途に
合わせた噴射速度で噴射推進します。燃焼ガス取出口８
８の、燃焼ガス温度を最低等に低下させて熱回収量を増
大し、燃焼ガス排気温度を−２７３℃に近付けます。そ
して海水等を冷却して、有害物質のＣＯ２等を大量の海
水に溶解し、海底などに冷熱として供給する過程で、霧
吹きの原理９１を利用して、酸素等を吸引して海中に供
給し、海の生物の生態を微生物まで徹底的に研究し、微
生物や魚介類や海草類や海藻類を繁殖させて、食料の増
産を図り、ＣＯ２等の燃焼ガス排気０を可能にします。Then, the combustion gas calorie output of the recovered calorie of about twice that of the existing boiler with the same fuel amount is supplied as steam 5 such as supercritical pressure, a part of which is supplied to the uppermost stream of the full-blade steam turbine to generate output. In the whole process of cooling the water jet steam, most of the steam velocity and the latent heat of vaporization are energy-converted into the atmospheric pressure 1700 times gravity power water mass velocity to generate the rotation output and the jet output most efficiently, and the jet output Is the levitation output. Then, the remaining superheated steam 5 to be used for bypass is injected, seawater or the like is sucked, and is propelled at an optimum speed. A water injection device 93a utilizing the spraying principle 91c, or a combustion gas 10 is injected to remove water in front. As a water injection device 93b that sucks and injects seawater etc. at an optimum speed to propel it, the water is propelled at an injection speed suited to the application. Combustion gas outlet 8
8 、 The combustion gas temperature is lowered to the minimum and the amount of heat recovery is increased to bring the combustion gas exhaust temperature close to -273 ° C. Then, in the process of cooling seawater, etc., dissolving harmful substances such as CO2 in a large amount of seawater, and supplying it as cold heat to the seabed, etc., oxygen is sucked and supplied into the sea by using the spraying principle 91. By thoroughly studying the ecology of marine organisms up to microorganisms, by breeding microorganisms, seafood, seaweeds, and seaweeds, we will increase the production of food and enable zero CO2 and other combustion gas emissions.

【００４２】図７・図８・図９・図１０を参照して、摩
擦ポンプ９７兼用の磁気摩擦動力伝達装置１４を説明す
る。通常の変速や逆転を含む各種動力伝達装置は、主と
して歯車装置を使用している。このため、歯面に大きな
荷重を含む、滑り歯面を必須とするため、潤滑油を必要
とするのに加えて、摩擦熱損失も非常に大きく、高速回
転を含む大動力の伝達装置には、使用不可という問題が
ある。このため、全動翼蒸気ガスタービン合体機関を実
用化するには、ころがり接触による、超高速大動力伝達
装置が必須です。超高速大動力伝達装置を可能にすると
共に、潤滑油も不用にするためには、歯車装置の滑り歯
面を皆無に近づけたころがり接触の、燃焼器兼熱交換器
に水冷却した摩擦熱を回収して供給する、多段多数で高
圧送水の、摩擦ポンプ９７と兼用の磁気摩擦動力伝達装
置として使用します。Referring to FIGS. 7, 8, 9 and 10, the magnetic friction power transmission device 14 which also serves as the friction pump 97 will be described. Various power transmission devices including normal gear shifting and reverse rotation mainly use gear devices. For this reason, a sliding tooth surface including a large load on the tooth surface is indispensable. Therefore, in addition to requiring lubricating oil, friction heat loss is also very large, and a large power transmission device including high speed rotation is required. There is a problem that it cannot be used. Therefore, in order to put a full-blade steam gas turbine combined engine into practical use, an ultra-high-speed large power transmission device by rolling contact is essential. In order to enable an ultra-high-speed large power transmission device and to eliminate the need for lubricating oil, water-cooled friction heat of the rolling contact with the sliding tooth surface of the gear device close to nothing is used for the combustor and heat exchanger. It is used as a magnetic friction power transmission device that is also used as the friction pump 97 for collecting and supplying multistage high pressure water.

【００４３】このため、歯車のかみ合い高さを限りなく
縮小した低凹凸４０として、転がり接触動力伝達装置と
し、回転方向３５上流側及び下流側、又は上流側又は下
流側に、棒磁石３３又は電磁石３４を設けます。そして
磁石の強い吸引力を利用して、各種着磁摩擦車装置５１
や、図にない各種磁着摩擦車装置９０や、各種内着磁摩
擦車装置４９や、図にない各種内磁着摩擦車装置８９等
の、すべての噛み合わせ使用を可能にします。高圧送水
摩擦ポンプ９７と兼用の各種磁気摩擦動力伝達装置１４
とし、外箱９４に吸水路９５や送水路９６を設けて、摩
擦ポンプ９７兼用として、公知技術を含めて全面的に使
用します。即ち、転がり接触に近付けて、摩擦熱損失を
大幅に低減し、更に高圧送水摩擦ポンプ９７と兼用とし
て熱回収する、超高速大動力を伝達する磁気摩擦動力伝
達装置１４や、潤滑油に換えて無公害の水冷却とし、熱
回収して燃焼器兼熱交換器４側に供給して使用する、摩
擦ポンプ９７兼用の磁気摩擦動力伝達装置１４とするも
のです。For this reason, as the low unevenness 40 in which the meshing height of the gear is reduced as much as possible, a rolling contact power transmission device is provided, and the bar magnet 33 or the electromagnet is provided on the upstream side and the downstream side in the rotation direction 35, or on the upstream side or the downstream side. 34 will be provided. Then, by utilizing the strong attractive force of the magnet, various magnetized friction wheel devices 51
It enables all meshing uses such as various magnetic friction friction wheel devices 90 (not shown), various inner magnetic friction friction wheel devices 49, and various inner magnetic friction friction wheel devices 89 (not shown). Various magnetic friction power transmission devices 14 which are also used as the high-pressure water supply friction pump 97
In addition, the outer box 94 is provided with a water absorption path 95 and a water supply path 96, and it is used as a friction pump 97 as a whole, including publicly known technology. That is, the magnetic friction power transmission device 14 for transmitting ultra-high speed and large power, which reduces the frictional heat loss significantly by approaching rolling contact and further recovers heat also as the high-pressure water supply friction pump 97, and replaces with lubricating oil It is a magnetic friction power transmission device 14 that also functions as a friction pump 97, which is used as water-cooled with no pollution, recovers heat, and supplies it to the combustor / heat exchanger 4 side for use.

【００４４】超高速大動力を伝達する、磁気摩擦動力伝
達装置１４とするためには、転がり接触に近付けても、
摩擦熱の発生を避けられません。一方全動翼蒸気ガスタ
ービン合体機関は、超高圧大量の水や熱を利用して出力
を発生させるため、超高速大動力を伝達すると共に、熱
回収して高圧送水する摩擦ポンプ９７が必要です。そこ
で各種歯車に換えて、各種着磁摩擦車３７や各種内着磁
摩擦車３８や、各種磁着摩擦車３９や図にない各種内磁
着摩擦車４４等を使用し、磁気摩擦動力伝達装置１４と
して使用の過程で、回転方向上流側及び下流側又は上流
側又は下流側に、棒磁石３３乃至電磁石３４を設けるこ
とで、着磁摩擦車や磁着摩擦車や内着磁摩擦車や内磁着
摩擦車の、すべての組み合わせを、磁石の強い吸引力に
より、互いに互換して使用を可能にした、摩擦ポンプ９
７兼用の磁気摩擦動力伝達装置１４とします。In order to make the magnetic friction power transmission device 14 which transmits super high speed and large power, even if it comes close to rolling contact,
The generation of frictional heat cannot be avoided. On the other hand, an all-blade steam gas turbine combined engine uses a large amount of ultra-high pressure water and heat to generate output, so it requires a friction pump 97 that transmits ultra-high speed power and recovers heat to deliver high-pressure water. . Therefore, in place of various gears, various magnetic friction wheels 37, various internal magnetic friction wheels 38, various magnetic friction wheels 39, various internal magnetic friction wheels 44 not shown, etc. are used. By providing bar magnets 33 to electromagnets 34 on the upstream side and the downstream side or the upstream side or the downstream side in the rotating direction in the process of use as 14, the magnetized friction wheel, the magnetized friction wheel, the inner magnetized friction wheel, and the inner magnetized friction wheel Friction pump 9 that enables all combinations of magnetic friction wheels to be used interchangeably due to the strong attractive force of the magnets
It is a magnetic friction power transmission device 14 that also serves 7.

【００４５】着磁摩擦車３７や磁着摩擦車３９や内着磁
摩擦車３８や内磁着摩擦車４４の、動力伝達面３１には
低凹凸４０を設けます。低凹凸４０は噛み合い高さを限
りなく低下させて、転がり接触として歯車以外の形状を
可能にし、図に無いすべての噛み合う形状全部としま
す。歯車形低凹凸４０として具体的には、平歯車に換え
て平凹凸４１車を、ハスバ歯車に換えてハスバ凹凸４２
車を、ヤマバ歯車に換えてヤマバ凹凸４３車を設ける。
又図に無い平内歯車に換えて平内凹凸４１ａ車を、ハス
バ内歯車に換えてハスバ内凹凸４２ａ車を、ヤマバ内歯
車に換えてヤマバ内凹凸４３ａ車を設ける。そして公知
の各種歯車ポンプと同様に、外箱９４や吸水路９５や送
水路９６を設けて、摩擦熱を回収して高圧送水する摩擦
ポンプ９７兼用として、超高速大動力を伝達する、摩擦
ポンプ９７兼用の各種磁気摩擦動力伝達装置１４として
使用します。A low unevenness 40 is provided on the power transmission surface 31 of the magnetized friction wheel 37, the magnetized friction wheel 39, the inner magnetized friction wheel 38, and the inner magnetized friction wheel 44. The low unevenness 40 reduces the meshing height as much as possible, and enables shapes other than gears as rolling contact, and makes all meshing shapes not shown in the figure. As the gear-shaped low unevenness 40, specifically, a flat unevenness 41 wheel is replaced with a spur gear and a helical unevenness 42 is replaced with a helical gear.
The car is replaced with a Yamaba gear and a Yamaba uneven 43 car is provided.
Further, instead of a plain internal gear (not shown), a plain internal concave-convex wheel 41a is provided, a helical internal gear 42a wheel is replaced with a helical internal gear, and a internal Yamaha concave 43a wheel is provided. As with various known gear pumps, an outer box 94, a water absorption path 95, and a water supply path 96 are provided to also serve as a friction pump 97 for recovering friction heat and supplying high-pressure water. It is used as various magnetic friction power transmission device 14 which also serves as 97.

【００４６】図７ａ・図７ｂの着磁摩擦車３７ａの実施
例は、環筒状の強磁性材料の径方向左右に磁極のＮ極及
びＳ極を着磁して、その両側を環板状のヨーク４７で挟
んで、外径方向動力伝達面３１に延長して固着します。
該動力伝達面３１の外周面に低凹凸４０の平凹凸４１や
ハスバ凹凸４２等を設けて、夫々着磁摩擦車３７ａ・３
７ａ等として、各要素を互いに互換して、着磁摩擦車３
７ａ・磁着摩擦車３９や、転がり接触の着磁摩擦車装置
５１とし、図８の着磁摩擦車装置５１ｃと同様に外箱９
４や吸水路９５や送水路９６等を設けて、摩擦ポンプ９
７兼用の各種磁気摩擦動力伝達装置１４として使用ま
す。In the embodiment of the magnetized friction wheel 37a shown in FIGS. 7a and 7b, the N and S poles of the magnetic poles are magnetized to the left and right in the radial direction of a ring-shaped ferromagnetic material, and both sides thereof are ring-shaped. It is sandwiched by the yoke 47 of and is extended and fixed to the outer diameter power transmission surface 31.
The outer peripheral surface of the power transmission surface 31 is provided with flat unevenness 41 of low unevenness 40, hasoba unevenness 42, and the like, and the magnetizing friction wheels 37a and 3a are respectively provided.
7a and the like, the respective elements are mutually compatible, and the magnetizing friction wheel 3
7a and the magnetic friction wheel 39 and the magnetic friction wheel device 51 for rolling contact, and the outer case 9 is the same as the magnetic friction wheel device 51c of FIG.
4, the water suction path 95, the water supply path 96, etc. are provided, and the friction pump 9
It is used as various magnetic friction power transmission device 14 for 7 uses.

【００４７】図７ｃの着磁摩擦車３７ｂの実施例は、環
筒状の強磁性材料の内径側と外径側に磁極のＮ極及びＳ
極を着磁して、ヨーク４７を磁石の内周側から左右外径
動力伝達面３１に延長します。該動力伝達面近傍のヨー
クと磁石の間に、摩擦増大手段４５を環状に設けて固着
し、その外周面に低凹凸４０のヤマバ凹凸４３を設け
て、夫々着磁摩擦車３７ｂ・３７ｂとして、各要素を互
いに互換して磁着摩擦車３９・着磁摩擦車３７ｂや、図
９の着磁摩擦車装置５１ｄと同様に外箱９４や吸水路９
５や送水路９６等を設けて、摩擦ポンプ９７兼用の各種
磁気摩擦動力伝達装置１４として使用します。The embodiment of the magnetizing friction wheel 37b shown in FIG. 7c is such that the N pole and the S pole of the magnetic poles are provided on the inner diameter side and the outer diameter side of the annular cylindrical ferromagnetic material.
Magnetize the poles and extend the yoke 47 from the inner circumference of the magnet to the left and right outer diameter power transmission surfaces 31. A friction increasing means 45 is provided in an annular shape between the yoke and the magnet in the vicinity of the power transmission surface, and is fixed to the magnet. Each element is compatible with each other, and the outer box 94 and the water absorption path 9 are similar to the magnetic friction wheel 39 / magnetization friction wheel 37b and the magnetic friction wheel device 51d of FIG.
5 and a water supply channel 96 are provided to be used as various magnetic friction power transmission devices 14 that also function as friction pumps 97.

【００４８】図７ｄ・図７ｅ・図７ｆの磁着摩擦車３９
の実施例は、環筒状の強磁性材料の外径面の動力伝達面
３１に、摩擦増大手段４５を設けます。又は動力伝達面
３１のまま、その外周面に低凹凸４０の平凹凸４１又は
ハスバ凹凸４２又はヤマバ凹凸４３を設けて、夫々各種
磁着摩擦車３９・３９等とします。夫々各要素を互いに
互換して、図に無い転がり接触の各種磁着摩擦車装置９
０とします。又は図にない環筒状の強磁性材料の内径面
の動力伝達面３１に、摩擦増大手段４５を設けます。又
は動力伝達面３１のまま、その内周面に低凹凸４０の平
凹凸４１又はハスバ凹凸４２又はヤマバ凹凸４３を設け
て、夫々各種内磁着摩擦車４４・４４等とします。夫々
各要素を互いに互換して、転がり接触の各種内磁着摩擦
車装置８９等とし、図８や図９や図１０の二重反転磁気
摩擦動力伝達装置１４と同様に外箱９４や多数の吸水路
９５や多数の送水路９６等を設けて、摩擦ポンプ９７兼
用の二重反転磁気摩擦動力伝達装置１４等として使用し
ます。The magnetic friction wheel 39 shown in FIGS. 7d, 7e and 7f.
In the embodiment, the friction increasing means 45 is provided on the power transmission surface 31 of the outer diameter surface of the annular cylindrical ferromagnetic material. Or, with the power transmission surface 31 as it is, the flat unevenness 41 of the low unevenness 40, the Hasuka unevenness 42 or the Yamaba unevenness 43 is provided on the outer peripheral surface thereof to form various magnetic friction wheels 39, 39, etc., respectively. Each element is compatible with each other, and various magnetic contact friction wheel devices 9 for rolling contact (not shown)
Set to 0. Alternatively, a friction increasing means 45 is provided on the power transmission surface 31 of the inner diameter surface of the annular cylindrical ferromagnetic material (not shown). Or, with the power transmission surface 31 as it is, by providing flat irregularities 41 of low irregularities 40, concavo-convex irregularities 42 or concavo-convex irregularities 43 on the inner peripheral surface thereof, various inner magnetic friction wheels 44, 44, etc. are provided. The respective elements are made compatible with each other to form various internal magnetic friction friction wheel devices 89, etc., which are in rolling contact with each other, and like the double-reversal magnetic friction power transmission device 14 of FIG. 8, FIG. 9 or FIG. The water absorption path 95 and a large number of water supply paths 96, etc. are provided to be used as the dual-reversal magnetic friction power transmission device 14 etc. that also functions as the friction pump 97.

【００４９】例えば図８・図９の摩擦ポンプ９７兼用の
各種磁気摩擦動力伝達装置の、第１実施例及び第２実施
例は、着磁摩擦車装置５１ｃ・５１ｄに、既存歯車ポン
プと同様に外箱９４を設け、夫々に吸水路９５及び送水
路９６を設けて、各種摩擦ポンプ９７を構成使用しま
す。そして吸水路９５より補給水を供給して、各種磁気
摩擦動力伝達装置１４で発生する熱を回収して、送水路
９６より燃焼器兼熱交換器４側に送水します。しかし着
磁摩擦車装置５１ｃ・５１ｄ等、多種多数の摩擦ポンプ
９７兼用の磁気摩擦動力伝達装置１４により、送水ポン
プ兼用となるのと動力伝達が主力のため、回転数も変化
します。そこで公知の制御装置により、１以上多数の送
水路９６や吸水路９５を最適制御して、１以上多段に昇
圧の過程で水噴射手段５６・５６ａに供給し、燃焼器兼
熱交換器４で超臨界圧力水蒸気等とします。即ち１以上
多数の摩擦ポンプ９７により、摩擦熱を回収して自己水
冷却し、超高速大動力を伝達しながら超高圧少量送水す
る、各種摩擦ポンプ９７兼用の、各種磁気摩擦動力伝達
装置１４として使用します。For example, in the first and second embodiments of the various magnetic friction power transmission devices which also function as the friction pump 97 of FIGS. 8 and 9, the magnetizing friction wheel devices 51c and 51d have the same structure as the existing gear pump. An outer box 94 is provided, and a water suction path 95 and a water supply path 96 are provided respectively, and various friction pumps 97 are used. Then, make-up water is supplied from the water absorption path 95 to recover the heat generated in the various magnetic friction power transmission devices 14 and to send it from the water supply path 96 to the combustor / heat exchanger 4 side. However, due to the magnetic friction power transmission device 14 that also serves as a large number of friction pumps 97, such as the magnetized friction wheel devices 51c and 51d, it also functions as a water pump, and because power transmission is the main force, the rotational speed also changes. Therefore, a well-known control device optimally controls one or more water supply paths 96 and water absorption paths 95 to supply water injection means 56, 56a to the water injection means 56 / 56a in the process of increasing the pressure in one or more stages, and the combustor / heat exchanger 4 Supercritical pressure steam, etc. That is, as various magnetic friction power transmission devices 14 also used as various friction pumps 97, which collects frictional heat by one or more friction pumps 97, cools water by itself, and transmits small amount of super high pressure while transmitting super high speed large power. To use.

【００５０】例えば、図１０の超高速大動力を伝達し
て、超高圧少量送水を可能する、摩擦ポンプ９７兼用の
二重反転磁気摩擦動力伝達装置１４は、外箱９４に多数
の吸水路９５及び多数の送水路９６及び多数の着磁摩擦
車３７ａ及び内着磁摩擦車３８ａ等で、多数の摩擦ポン
プ９７が構成されるため、外箱９４も非常に複雑になり
ます。しかし着磁摩擦車３７ａの周速度は２種類のた
め、同じ周速度のものを合流して、この場合は２段に昇
圧して圧力制御し、用途に合わせて他の摩擦ポンプとも
組み合わせて、燃焼器兼熱交換器４側に給水します。多
数の摩擦ポンプ９７により摩擦熱を回収して自己水冷却
し、超高速大動力を伝達する、摩擦ポンプ９７兼用の各
種磁気摩擦動力伝達装置１４として使用します。For example, the double-reversal magnetic friction power transmission device 14 also serving as the friction pump 97, which transmits the ultra-high speed and large power in FIG. Also, since the many friction pumps 97 are composed of many water supply channels 96, many magnetized friction wheels 37a and inner magnetized friction wheels 38a, etc., the outer box 94 also becomes very complicated. However, since the peripheral speeds of the magnetized friction wheel 37a are two types, those having the same peripheral speed are merged, and in this case, the pressure is controlled by increasing the pressure in two stages, and in combination with other friction pumps according to the application, Water is supplied to the combustor / heat exchanger 4 side. It is used as a variety of magnetic friction power transmission device 14 that also serves as a friction pump 97, which collects friction heat by a large number of friction pumps 97, cools itself with water, and transmits ultra-high speed large power.

【００５１】図１０（ａ）（ｂ）（ｃ）を参照して説明
する。（ｂ）（ｃ）は夫々（ａ）のｃ−ｃ及びｄ−ｄ視
図であり、互いに反対方向に回転する全動翼蒸気ガスタ
ービン合体機関の、内側軸装置と外側軸装置の回転動力
を結合する、二重反転磁気摩擦動力伝達装置１４を、図
１０の実施例により説明する。図１０（ａ）は、多数の
摩擦ポンプ９７により摩擦熱を回収して自己水冷却し、
超高速大動力を伝達する、二重反転磁気摩擦動力伝達装
置１４として使用します。全動翼蒸気ガスタービン合体
機関の外側軸装置に固着された、磁石部４６及びヨーク
４７を含む、第一主動内着磁摩擦車３８ａの回転によ
り、機関本体に固定された外箱９４に軸支された、支軸
５０の左端に固着された複数の第一従動着磁摩擦車３７
ａが回転し、その回転により支軸５０の右端に固着し
た、複数の第二主動着磁摩擦車３７ａが回転し、その回
転により内側軸装置に固着された、第二従動着磁摩擦車
３７ａが回転して、互いに反対方向に回転する外側軸装
置の回転力と、内側軸装置の回転力を結合して、内側軸
装置又は外側軸装置より全回転出力を、取り出し可能と
します。Description will be made with reference to FIGS. 10 (a), 10 (b) and 10 (c). (B) and (c) are cc and dd views of (a), respectively, and are rotational powers of the inner shaft device and the outer shaft device of the full-blade steam gas turbine combined engine rotating in opposite directions. The counter-rotating magnetic friction power transmission device 14 for coupling the above will be described with reference to the embodiment of FIG. In FIG. 10A, friction heat is collected by a large number of friction pumps 97 and self-cooled by water,
It is used as a double-reversal magnetic friction power transmission device 14 that transmits super high speed and large power. The rotation of the first drive internal magnetizing friction wheel 38a, which includes the magnet portion 46 and the yoke 47 and is fixed to the outer shaft device of the all-blade steam gas turbine integrated engine, causes the outer box 94 fixed to the engine body to rotate in the shaft. A plurality of first driven magnetized friction wheels 37 fixed to the left end of the support shaft 50.
a rotates, and by the rotation, a plurality of second main drive magnetized friction wheels 37a fixed to the right end of the support shaft 50 rotate and the second driven magnetic friction wheels 37a fixed to the inner shaft device by the rotation. The rotation force of the outer shaft device that rotates in the opposite direction and the rotation force of the inner shaft device are combined, and the full rotation output can be taken out from the inner shaft device or the outer shaft device.

【００５２】図１０（ｂ）（ｃ）は、超高速大動力を伝
達と超高圧少量送水する、摩擦ポンプ９７兼用の二重反
転磁気摩擦動力伝達装置１４として使用の過程で、回転
方向上流側及び下流側又は上流側又は下流側に、棒磁石
３３乃至電磁石３４を設けることで、着磁摩擦車３７や
磁着摩擦車３９や内着磁摩擦車３８や内磁着摩擦車４４
の、すべての組み合わせを、磁石の強い吸引力により、
互いに互換して使用を可能にします。外側軸装置に固着
の内着磁摩擦車３８ａや、内側軸装置に固着の着磁摩擦
車３７ａや、夫々に噛み合う夫々複数の着磁摩擦車３７
ａを含めて、既存歯車ポンプと同様に外箱９４を設けま
す。そして内着磁摩擦車３８ａに噛み合う複数の着磁摩
擦車３７ａの、回転方向棒磁石３３を含む上流側に送水
路９６を設け、回転方向棒磁石３３を含む下流側に吸水
路９５を設け、内側軸装置に固着の着磁摩擦車３７ａに
噛み合う複数の着磁摩擦車３７ａの、回転方向電磁石３
４を含む上流側に送水路９６を設け、回転方向電磁石３
４を含む下流側に吸水路９５を設けて、摩擦ポンプ９７
兼超高速大動力を伝達する、摩擦ポンプ９７兼用の二重
反転磁気摩擦動力伝達装置１４を構成します。FIGS. 10 (b) and 10 (c) show the upstream side in the rotating direction in the process of use as the double-reversal magnetic friction power transmission device 14 that also transmits the ultra-high speed large power and the ultra-high pressure small amount of water and also serves as the friction pump 97. By providing the bar magnets 33 to the electromagnets 34 on the downstream side, the upstream side, or the downstream side, the magnetizing friction wheel 37, the magnetic friction wheel 39, the inner magnetizing friction wheel 38, or the inner magnetizing friction wheel 44.
All combinations of the
Enables compatibility with each other. An inner magnetized friction wheel 38a fixed to the outer shaft device, a magnetized friction wheel 37a fixed to the inner shaft device, and a plurality of magnetized friction wheels 37 that mesh with each other.
Outer box 94 is installed in the same way as the existing gear pump including a. A plurality of magnetizing friction wheels 37a meshing with the inner magnetizing friction wheel 38a are provided with a water supply path 96 on the upstream side including the rotating direction bar magnet 33, and a water absorbing path 95 is provided on the downstream side including the rotating direction bar magnet 33. Rotational direction electromagnet 3 of a plurality of magnetizing friction wheels 37a meshing with the magnetizing friction wheel 37a fixed to the inner shaft device.
4, a water passage 96 is provided on the upstream side, and the rotation direction electromagnet 3
4, the water absorption path 95 is provided on the downstream side, and the friction pump 97
It also composes a dual-reversal magnetic friction power transmission device 14 that also serves as a friction pump 97 and transmits ultra-high speed large power.

【００５３】図１１の全動翼蒸気ガスタービン合体機関
の、回転力や噴射出力で駆動する、各種装置を説明す
る。燃焼ガス質量出力で駆動の全動翼ガスタービンは、
主に冷熱回収特殊用途用として、燃焼ガス排気温度を−
２７３℃に近付け、極低温燃焼ガスを核に水や水蒸気等
を凝集して、雹等として排出することで、冷熱やＣＯ２
等の回収を容易とし、用途に合わせてＣＯ２等の燃焼ガ
ス排気を０にします。燃焼ガス熱量出力の水蒸気は、全
動翼蒸気タービンにより膨大な電力量等に、主として変
換使用します。又全動翼蒸気ガスタービン乃至全動翼蒸
気ガスタービン合体機関として、構造を大幅に簡単と
し、大部分の回転出力の用途に対応します。又水蒸気や
燃焼ガスをバイパス噴射使用する、霧吹きの原理を利用
して噴射推進も含めたものが、各種全動翼蒸気ガスター
ビン合体機関となります。回転力や噴射推進出力で駆動
する各種装置を、発電設備・熱と電気と冷熱の供給設備
・熱と電気の供給設備・各種船舶・各種高速船舶・各種
飛行機・各種汎用機関・各種自動車・各種車両・各種機
械・各種艦船・各種戦闘機・各種戦車・宇宙往還親飛行
機・超音速機・飛行機器等とします。Various devices which are driven by the rotational force and the injection output of the all-blade steam gas turbine combined engine of FIG. 11 will be described. An all-blade gas turbine driven by combustion gas mass output
Combustion gas exhaust gas temperature-
By bringing it close to 273 ° C and coagulating water, water vapor, etc. in the core of the cryogenic combustion gas and discharging it as hail etc., cold heat and CO2
Etc. facilitates the recovery of CO2, etc., and reduces the exhaust gas of combustion gas such as CO2 to 0 according to the application. Steam of combustion gas calorific value output is mainly converted and used for huge amount of electric power etc. by all moving blade steam turbine. Also, as a full moving blade steam gas turbine or a full moving blade steam gas turbine united engine, the structure is greatly simplified and it corresponds to most rotary output applications. In addition, various full-blade steam gas turbine integrated engines include injection propulsion using the principle of mist blowing, which uses steam and combustion gas by-pass injection. Various devices driven by rotational force and injection propulsion output are used for power generation equipment, heat, electricity and cold supply equipment, heat and electricity supply equipment, various vessels, various high speed vessels, various airplanes, various general-purpose engines, various automobiles, various Vehicles, various machines, various ships, various fighters, various tanks, space shuttle parent planes, supersonic planes, airplanes, etc.

【００５４】[0054]

【発明の効果】本発明は、各種全動翼蒸気ガスタービン
合体機関の全動翼圧縮機の、撥水性水冷却翼８７で構成
の、外側圧縮機動翼郡１６及び内側圧縮機動翼郡１７
を、水冷却して圧縮空気容積を縮小し、低温空気とする
過程を、全動翼圧縮機の撥水性水冷却翼８７を水冷却し
た水を、更に水噴射手段５６より噴射して、圧縮空気を
直接水冷却して低温空気とし、熱回収して昇温した水を
燃焼器兼熱交換器４側に供給します。即ち、撥水性水冷
却翼８７で構成することで摩擦損失を低減し、最も効率
よく圧縮して空気を冷却し、熱回収量を増大する効果が
あります。INDUSTRIAL APPLICABILITY The present invention includes a group 16 of outer compressor blades and a group 17 inner compressor blades which are composed of water repellent water cooling blades 87 of all rotor blade compressors of various rotor blade steam gas turbine integrated engines.
Is cooled with water to reduce the volume of compressed air into low-temperature air. In the process of water-cooling the water-repellent water-cooling blades 87 of the full-blade compressor, water is further injected from the water injection means 56 to compress the water. The water is cooled directly with water to form low-temperature air, and the water that has recovered heat and heated is supplied to the combustor / heat exchanger 4 side. In other words, the water-repellent water cooling blade 87 has the effect of reducing friction loss, compressing the air most efficiently and cooling the air, and increasing the amount of heat recovery.

【００５５】撥水性タービン翼８１及び撥水性噴口８３
を、加熱高温・撥水性金属・撥水性物質の被覆・撥水性
セラミックス・撥水性加工の、何れか１以上で構成の撥
水性全動翼タービン翼とし、水等との摩擦損失・消費熱
量を僅少とします。そして段落毎環状に撥水性タービン
翼８１を一体鋳造として、その全部乃至一部を、電気絶
縁した電線の配線を鋳込む等で、容易確実に加熱高温に
する効果があります。断熱して設けた水噴射手段５６ａ
の鋳込みにより、水噴射して燃焼ガスや水蒸気を冷却
し、単位容積質量や全質量の増大を、確実容易にする効
果があります。従って、燃焼ガス排気温度を−２７３℃
に近付けて、大きな単位重力パワーや全重力パワーにし
ても、撥水性タービン翼等と水等との摩擦損失最小・消
費熱量最少で、大きな出力を発生させる効果がありま
す。Water-repellent turbine blade 81 and water-repellent nozzle 83
Is a water-repellent full-rotor turbine blade composed of at least one of high-temperature heating, water-repellent metal, water-repellent substance coating, water-repellent ceramics, and water-repellent finish, and reduces friction loss and heat consumption with water, etc. It will be very small. The water-repellent turbine blade 81 is integrally cast in an annular shape for each paragraph, and the whole or a part of it is cast with the wire of the electrically insulated electric wire, which has the effect of easily and surely heating to high temperature. Water jetting means 56a provided with heat insulation
By casting, the water is injected to cool the combustion gas and steam, which has the effect of making it easy to increase the unit volume mass and total mass. Therefore, set the combustion gas exhaust temperature to -273 ° C.
Even with a large unit gravity power or total gravity power, it has the effect of generating a large output with minimum friction loss between the water repellent turbine blade and water and the minimum heat consumption.

【００５６】低温高圧空気を燃焼器兼熱交換器で、限り
なく燃焼熱交換することで、理論空燃比まで燃料燃焼質
量を、従来ガスタービンの４倍前後に増大を可能とし、
全動翼蒸気ガスタービンや全動翼ガスタービンの燃焼ガ
ス入口温度や、全動翼蒸気タービンの燃焼器兼熱交換器
の燃焼ガス出口温度を、最低としたため圧縮圧力を２倍
前後の１０ＭＰａ以上を可能にします。そして熱交換し
て得た燃焼ガス熱量に、圧縮空気−２７３℃以上略全部
を加えて、同一燃料量既存ボイラの２倍前後の燃焼ガス
熱量の回収として、全動翼蒸気タービンや全動翼蒸気ガ
スタービンや、特殊装置９２ａ・９２ｂや水噴射装置９
３ａ・９３ｂを駆動します。そして燃焼ガス排気温度を
−２７３℃に近付けて、全動翼ガスタービンの燃焼ガス
質量出力を既存ガスタービンの４倍乃至６倍等として、
該消費燃料燃焼ガス熱量を０以下等に近付け、該熱効率
を無限上昇に近付ける効果があります。By infinitely exchanging combustion heat with low-temperature high-pressure air in the combustor and heat exchanger, it is possible to increase the fuel combustion mass up to the theoretical air-fuel ratio by about 4 times that of the conventional gas turbine.
Since the combustion gas inlet temperature of the all-blade steam gas turbine and all-blade gas turbine and the combustion gas outlet temperature of the combustor / heat exchanger of the all-blade steam turbine are the lowest, the compression pressure is doubled to 10 MPa or more. make it possible. Then, to the combustion gas heat quantity obtained by heat exchange, almost all compressed air -273 ° C or more is added to recover the combustion gas heat quantity about twice as much as that of the existing boiler with the same fuel amount. Steam gas turbine, special equipment 92a / 92b and water injection device 9
Drives 3a and 93b. Then, the combustion gas exhaust temperature is brought close to -273 ° C., and the combustion gas mass output of the full-blade gas turbine is set to 4 to 6 times that of the existing gas turbine,
It has the effect of making the consumed fuel combustion gas calorific value close to 0 or less and making the thermal efficiency near infinite increase.

【００５７】水噴射水蒸気や燃焼ガスを冷却して、速度
を重力パワーにエネルギ変換して、大気圧重力パワー１
７００倍凝縮水を創出増大することで、全動翼蒸気ガス
タービンや全動翼ガスタービンをコンパクトに設計でき
る大きな効果があります。既存技術の最悪を逆転して最
良にすることで、電気料金を低下させて、発電所等から
排出されるＣＯ２等の地球温暖化燃焼ガスを、最も効率
良く回収する効果もあります。そして事業用クーラーや
家庭用クーラーを全廃して、脱フロンによる地球温暖化
防止の効果もあります。発電量を増大する程極低温燃焼
ガスの増産になるため、海水を冷却すると海底にＣＯ２
や窒素や酸素を供給して、海藻や魚類等を繁殖させて活
性化する効果があります。金儲けのみが企業活動と感え
る誤りを逆転して、人類のために貢献する手法を皆で考
える効果があります。Water jet Water vapor and combustion gas are cooled, the velocity is converted into gravity power, and atmospheric pressure gravity power 1
By creating and increasing 700 times the condensed water, there is a great effect that the all-blade steam gas turbine and all-blade gas turbine can be designed compactly. By reversing the worst of the existing technology and making it the best, it also has the effect of lowering the electricity bill and recovering the global warming combustion gas such as CO2 emitted from power plants etc. most efficiently. It also has the effect of preventing global warming by eliminating CFCs by completely eliminating commercial and domestic coolers. As the amount of power generation increases, the production of cryogenic combustion gas increases, so when seawater is cooled, CO2
It also has the effect of supplying nitrogen and oxygen to reproduce and activate seaweed and fish. It is effective for everyone to think about how to contribute to the benefit of mankind by reversing the error that only money-making can be perceived as corporate activity.

【００５８】本発明は、各種全動翼蒸気ガスタービン合
体機関の燃焼器兼熱交換器で、限りなく燃焼熱交換する
ことで、理論空燃比まで燃料燃焼質量を、従来ガスター
ビンの４倍前後を可能とします。全動翼ガスタービンや
全動翼蒸気ガスタービンの、燃焼ガス入口温度を最低と
したため、圧力比を２倍前後の１０ＭＰａ以上を可能と
して、燃焼器兼熱交換器で熱交換して得た、燃焼ガスや
水蒸気を水冷却し、単位重力パワーが既存蒸気タービン
の大気圧１７００倍、真空部１００００倍以上の水質量
を最大最適に増大します。従って、既存蒸気タービン過
熱蒸気の１７００倍や１００００倍の、大きな動圧によ
り出力を発生出来る大きな効果があります。又重力パワ
ーを１７００倍や１００００倍に増大することで、ター
ビン動翼面積の一部乃至大部分を、１／１７００や１／
１００００等に縮小して、構造を大幅に簡単に出来る大
きな効果があります。The present invention is a combustor and heat exchanger for various all-blade steam gas turbine coalescing engines, and by infinitely exchanging combustion heat, the fuel combustion mass up to the theoretical air-fuel ratio is about four times that of the conventional gas turbine. It is possible. Since the combustion gas inlet temperature of all moving blade gas turbines and all moving blade steam gas turbines was set to the minimum, it was possible to obtain a pressure ratio of about 10 MPa or more, which was about twice, and obtained heat by exchanging heat with a combustor and heat exchanger. By cooling the combustion gas and steam with water, the unit gravity power maximizes the maximum water mass of 1700 times the atmospheric pressure and 10000 times the vacuum part of the existing steam turbine. Therefore, there is a great effect that the output can be generated by a large dynamic pressure that is 1700 times or 10000 times that of the existing steam turbine superheated steam. Also, by increasing the gravity power to 1700 times or 10000 times, a part or most of the turbine blade area can be reduced to 1/1700 or 1 /
There is a great effect that the structure can be greatly simplified by reducing it to 10000 mag.

【００５９】既存再熱蒸気タービンの再熱や静翼を全廃
して、構造を全動翼小型簡単大出力に出来る大きな効果
があります。全動翼蒸気ガスタービンや、全動翼ガスタ
ービンの出力発生の過程で、水噴射水蒸気や燃焼ガスを
冷却して、水質量を増大するため、断熱膨張極低温燃焼
ガスを核に水や水蒸気を凝集して、自然現象と同様に雹
や水滴等として、膨大な水等にＣＯ２等の燃焼ガスを合
成溶解混合する過程で、物質を加えて無害で排出可能に
する効果もあります。各種自動車や各種船舶や各種飛行
機や、各種機械装置等から排出されける、ＣＯ２等の公
害燃焼ガス排気を、雹や水滴として排出して、０等に大
幅に低減する効果があります。Reheat of the existing reheat steam turbine and total elimination of the stationary blades have the great effect that the structure can be reduced to all moving blades, small size, simple and large output. In the process of generating the output of an all-blade steam gas turbine or an all-blade gas turbine, in order to increase the water mass by cooling the water-injected steam and the combustion gas, the adiabatic expansion cryogenic combustion gas is used as the core for water and steam. It also has the effect of adding substances and harmlessly discharging them in the process of synthetically dissolving and mixing combustion gases such as CO2 into a huge amount of water, such as hail and water droplets, similar to natural phenomena. It has the effect of significantly reducing CO2 and other pollutant combustion gas exhausts emitted from various automobiles, various ships, various airplanes, various mechanical devices, etc. as hail and water drops to 0.

【００６０】本発明最大の効果は、既存最先端再熱蒸気
タービン技術では、出力発生の過程で、過熱蒸気の大き
な動圧により、タービン動翼や静翼表面の飽和温度が飛
躍的に上昇するため、いくら再熱しても湿り蒸気（凝縮
水）となって、膨大な面積の摩擦損失増大を避けられま
せん。最大の問題は、再熱により容積が真空部１０００
０倍以上に増大するため、落差×質量が一定のまま、単
位重力パワーが初段の１／１００００以下に減少し、真
空部動翼面積の１００００倍増等が必要となり、静翼を
設ける等無茶苦茶設計となって、摩擦損失は１００倍等
に、大幅に増大します。そこで本発明は、再熱を逆転し
て水蒸気を水噴射冷却し、単位重力パワー大気圧部既存
技術の１７００倍、真空部１００００倍以上の水質量を
最大最適に増大します。そして撥水性タービン翼と水等
との間の摩擦損失を最少に、消費熱量も最少で２００倍
等の出力に、大幅に増大する大きな効果があります。The greatest effect of the present invention is that in the existing state-of-the-art reheat steam turbine technology, the saturation temperature of the turbine rotor blades and the stator blade surface rises dramatically due to the large dynamic pressure of the superheated steam in the process of power generation. Therefore, no matter how many times it is reheated, it becomes wet steam (condensed water), and inevitably an increase in friction loss over a huge area. The biggest problem is that the volume is reduced to 1000 by reheating.
Since it increases more than 0 times, the unit gravity power decreases to 1/10000 or less of the first stage while the head x mass remains constant, and it is necessary to increase the vacuum blade area by 10,000 times. The tea design increases friction loss by 100 times. Therefore, the present invention reverses reheat to inject and cool water vapor to increase optimally the water mass of 1700 times more than existing technology of unit gravity power atmospheric pressure section and 10,000 times more than vacuum section. And it has the great effect that the friction loss between the water-repellent turbine blade and water is minimized and the heat consumption is minimized to 200 times or more.

【図面の簡単な説明】[Brief description of drawings]

【図１】全動翼ガスタービンの実施例を示す一部断面
図。FIG. 1 is a partial cross-sectional view showing an embodiment of a full-blade gas turbine.

【図２】全動翼蒸気タービンの第１実施例を示す一部断
面図。FIG. 2 is a partial cross-sectional view showing a first embodiment of a full-blade steam turbine.

【図３】全動翼蒸気ガスタービンの第１実施例を示す一
部断面図。FIG. 3 is a partial cross-sectional view showing a first embodiment of a full-blade steam gas turbine.

【図４】全動翼蒸気ガスタービンの第２実施例を示す一
部断面図。FIG. 4 is a partial cross-sectional view showing a second embodiment of the full-blade steam gas turbine.

【図５】全動翼蒸気タービンの第２実施例を示す一部断
面図。FIG. 5 is a partial cross-sectional view showing a second embodiment of the full-blade steam turbine.

【図６】全動翼蒸気タービンの第３実施例を示す一部断
面図。FIG. 6 is a partial sectional view showing a third embodiment of a full-blade steam turbine.

【図７】着磁摩擦車及び磁着摩擦車の実施例を示す一部
断面図。FIG. 7 is a partial cross-sectional view showing an embodiment of a magnetized friction wheel and a magnetized friction wheel.

【図８】摩擦ポンプ兼用の磁気摩擦動力伝達装置の第１
実施例の一部断面図。FIG. 8 shows a first magnetic friction power transmission device which also functions as a friction pump.
The partial cross section figure of an Example.

【図９】摩擦ポンプ兼用の磁気摩擦動力伝達装置の第２
実施例の一部断面図。FIG. 9 is a second part of a magnetic friction power transmission device which is also used as a friction pump.
The partial cross section figure of an Example.

【図１０】摩擦ポンプ兼用の二重反転磁気摩擦動力伝達
装置の実施例の一部断面図。FIG. 10 is a partial cross-sectional view of an embodiment of a counter-rotating magnetic friction power transmission device that also serves as a friction pump.

【図１１】全動翼蒸気ガスタービン合体機関で駆動する
装置を示す説明図。FIG. 11 is an explanatory diagram showing a device driven by a combined rotor and gas turbine integrated engine.

【符号の説明】[Explanation of symbols]

１：導水管 ２：給水ポンプ ３：給水 ４：燃
焼器兼熱交換器 ５：水蒸気 ６：蒸気管 ７：
蒸気加減弁 ８：環状の圧縮空気溜 ９：環状の燃
焼ガス溜 １０燃焼ガス １１：燃料 １２：出
力軸 １３：止め弁 １４：磁気摩擦動力伝達装置
１５：圧縮空気 １６：外側圧縮機動翼群 １
７：内側圧縮機動翼群 １９：外側タービン動翼群
２０：内側タービン動翼群 ２１：環状の出口
２２：環状の受け口 ２３：環状の受け口 ２４：
環状の撥水性噴口群 ２５：燃焼器外箱部 ２６：
水冷外壁 ２７：燃料蒸気供給手段 ２８：バイパ
ス ３１：動力伝達面 ３２：過熱蒸気溜 ３３：棒磁石 ３４：電磁石
３５：回転方向 ３６：磁極 ３７：着磁摩擦車 ３８：内着磁摩擦
車 ３９：磁着摩擦車 ４０：低凹凸 ４１：平凹凸 ４２：ハスバ凹凸
４３：ヤマバ凹凸 ４４：内磁着摩擦車 ４５：摩擦増大耐久手段 ４
６：磁石部 ４７：ヨーク（着磁摩擦車用） ４
８：絶縁材料 ４９ａ：内着磁摩擦車装置 ４９ｂ：内着磁摩擦車装置 ５０：支軸 ５１ａ：
着磁摩擦車装置 ５１ｂ：着磁摩擦車装置 ５１
ｃ：着磁摩擦車装置 ５１ｄ：着磁摩擦車装置 ５２：水冷外壁単位 ５３：鍔 ５４：水冷内壁
５５：冷却手段 ５６：水噴射手段 ５６ａ：水噴射手段 ５７：毛
細管放出手段 ５８：排気熱交換器 ５９：過熱蒸
気筒口 ６０：燃料噴口 ６１：針弁 ６２：燃料*** ６３：燃料穴開閉器 ６４：空気
穴開閉器 ６５：空気穴 ６６：凝縮水熱交換器
６７：復水器 ６８：凝縮水 ６９：排気 ７０：水道水 ７１：温熱 ７２：冷熱 ７３：
冷却水 ７４：推力 ７９：加熱高温手段 ８
０：ヨーク ８１：撥水性タービン翼 ８３：撥水
性噴口 ８４：環状に一体鋳造 ８５：外径組立環
状部 ８６：内径組立環状部 ８７：撥水性水冷却
翼 ８８：燃焼ガス取出口 ８９：内磁着摩擦車装
置 ９０：磁着摩擦車装置 ９１ａ：霧吹きの原理
９１ｂ：霧吹きの原理 ９１ｃ：霧吹きの原理
９１ｄ：霧吹きの原理 ９２ａ：特殊装置 ９２
ｂ：特殊装置 ９３ａ：水噴射装置 ９３ｂ：水噴
射装置 ９４：外箱 ９５：吸水路 ９６：送水
路 ９７：摩擦ポンプ1: Water conduit 2: Water supply pump 3: Water supply 4: Combustor / heat exchanger 5: Water vapor 6: Steam pipe 7:
Steam control valve 8: Annular compressed air reservoir 9: Annular combustion gas reservoir 10 Combustion gas 11: Fuel 12: Output shaft 13: Stop valve 14: Magnetic friction power transmission device 15: Compressed air 16: Outer compressor blade group 1
7: Inner compressor blade group 19: Outer turbine blade group
20: Inner turbine blade group 21: Annular outlet
22: Annular socket 23: Annular socket 24:
Ring-shaped water-repellent jet group 25: Combustor outer box 26:
Water-cooled outer wall 27: Fuel vapor supply means 28: Bypass 31: Power transmission surface 32: Superheated vapor reservoir 33: Bar magnet 34: Electromagnet
35: Rotation direction 36: Magnetic pole 37: Magnetization friction wheel 38: Inner magnetization friction wheel 39: Magnetization friction wheel 40: Low unevenness 41: Flat unevenness 42: Haska unevenness
43: Yamaba unevenness 44: Inner magnetic friction wheel 45: Friction increasing durability means 4
6: Magnet part 47: Yoke (for magnetized friction wheel) 4
8: Insulating material 49a: Inner magnetized friction wheel device 49b: Inner magnetized friction wheel device 50: Spindle 51a:
Magnetizing friction wheel device 51b: Magnetizing friction wheel device 51
c: Magnetizing friction wheel device 51d: Magnetizing friction wheel device 52: Water-cooled outer wall unit 53: Tsubo 54: Water-cooled inner wall
55: Cooling means 56: Water injection means 56a: Water injection means 57: Capillary discharge means 58: Exhaust heat exchanger 59: Superheated steam cylinder port 60: Fuel injection port 61: Needle valve 62: Fuel small hole 63: Fuel hole switch 64: Air hole switch 65: Air hole 66: Condensate heat exchanger
67: Condenser 68: Condensed water 69: Exhaust gas 70: Tap water 71: Hot heat 72: Cold heat 73:
Cooling water 74: Thrust 79: Heating high temperature means 8
0: Yoke 81: Water-repellent turbine blade 83: Water-repellent injection port 84: Ring-shaped integral casting 85: Outer diameter assembled annular portion 86: Inner diameter assembled annular portion 87: Water-repellent water cooling blade 88: Combustion gas outlet 89: Inner magnet Friction wheel device 90: Magnetic friction wheel device 91a: Principle of spraying 91b: Principle of spraying 91c: Principle of spraying
91d: Principle of spraying 92a: Special device 92
b: Special device 93a: Water injection device 93b: Water injection device 94: Outer box 95: Water absorption path 96: Water supply path 97: Friction pump

───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.⁷ 識別記号 ＦＩ テーマコート゛(参考） Ｆ０１Ｋ 23/06 Ｆ０１Ｋ 27/02 Ｃ 27/02 Ｆ０２Ｃ 3/073 Ｆ０２Ｃ 3/073 3/30 Ｚ 3/30 Ｆ０２Ｇ 5/04 Ｈ Ｆ０２Ｇ 5/04 Ｆ１６Ｈ 49/00 Ａ Ｆ１６Ｈ 49/00 Ｂ０１Ｄ 53/34 １３５Ｚ Ｆターム(参考） 3G002 CA02 CA07 CA13 CB01 EA05 EA06 EA08 3G081 BA02 BA11 BB00 BC04 DA07 DA23 4D002 AA09 AC01 BA02 BA13 CA01 DA35 EA02 GA02 GB02 ─────────────────────────────────────────────────── ─── Continuation of front page (51) Int.Cl. ⁷ Identification code FI theme code (reference) F01K 23/06 F01K 27/02 C 27/02 F02C 3/073 F02C 3/073 3/30 Z 3/30 F02G 5/04 H F02G 5/04 F16H 49/00 A F16H 49/00 B01D 53/34 135Z F term (reference) 3G002 CA02 CA07 CA13 CB01 EA05 EA06 EA08 3G081 BA02 BA11 BB00 BC04 DA07 DA23 4D002 AA09 AC01 BA35 BA13 CA13 BA02 BA13 CA13 EA02 GA02 GB02

Claims (332)

【特許請求の範囲】[Claims] 【請求項１】 摩擦ポンプ（９７）兼用の磁気摩擦動力
伝達装置（１４）により互いに反対方向に回転する外側
軸装置と内側軸装置を、最適回転比で結合した全動翼ガ
スタービンのタービン翼を撥水性としたことが特徴の全
動翼蒸気ガスタービン合体機関。1. A turbine blade of a rotor blade gas turbine in which an outer shaft device and an inner shaft device that rotate in mutually opposite directions by a magnetic friction power transmission device (14) that also serves as a friction pump (97) are connected at an optimum rotation ratio. An all-blade steam-gas turbine united engine characterized by water repellency. 【請求項２】 摩擦ポンプ（９７）兼用の磁気摩擦動力
伝達装置（１４）により互いに反対方向に回転する外側
軸装置と内側軸装置を、最適回転比で結合した全動翼蒸
気ガスタービンのタービン翼を撥水性としたことを特徴
とする全動翼蒸気ガスタービン合体機関。2. A turbine of a full-blade steam gas turbine in which an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also serves as a friction pump (97) are connected at an optimum rotation ratio. An all-blade steam gas turbine united engine characterized by having water-repellent blades. 【請求項３】 摩擦ポンプ（９７）兼用の磁気摩擦動力
伝達装置（１４）により互いに反対方向に回転する外側
軸装置と内側軸装置を、最適回転比で結合した全動翼蒸
気タービンのタービン翼を撥水性としたことが特徴の全
動翼蒸気ガスタービン合体機関。3. A turbine blade of a full-blade steam turbine in which an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also serves as a friction pump (97) are connected at an optimum rotation ratio. An all-blade steam-gas turbine united engine characterized by water repellency. 【請求項４】 摩擦ポンプ（９７）兼用の磁気摩擦動力
伝達装置（１４）により互いに反対方向に回転する外側
軸装置と内側軸装置を最適回転比で結合し、撥水性ター
ビン翼を具備した全動翼ガスタービンにおいて、環状に
一体鋳造（８４）して組立構造とした夫々の外側タービ
ン動翼群（１９）及び内側タービン動翼群（２０）とし
たことを特徴とする全動翼蒸気ガスタービン合体機関。4. A magnetic repulsive power transmission device (14) which also serves as a friction pump (97) is used to couple an outer shaft device and an inner shaft device rotating in opposite directions to each other at an optimum rotation ratio, and a water repellent turbine blade is provided. In a rotor blade gas turbine, a total rotor blade steam gas, characterized in that an outer casting rotor blade group (19) and an inner turbine rotor blade group (20) are integrally cast in an annular shape (84) into an assembled structure. Turbine united engine. 【請求項５】 摩擦ポンプ（９７）兼用の磁気摩擦動力
伝達装置（１４）により互いに反対方向に回転する外側
軸装置と内側軸装置を最適回転比で結合し、撥水性ター
ビン翼を具備した全動翼蒸気ガスタービンにおいて、環
状に一体鋳造（８４）して組立構造とした夫々の外側タ
ービン動翼群（１９）及び内側タービン動翼群（２０）
としたことを特徴とする全動翼蒸気ガスタービン合体機
関。5. A magnetic friction power transmission device (14) that also serves as a friction pump (97) is used to connect an outer shaft device and an inner shaft device that rotate in mutually opposite directions at an optimum rotation ratio, and a water repellent turbine blade is provided. In a moving blade steam gas turbine, an outer turbine moving blade group (19) and an inner turbine moving blade group (20) are integrally cast (84) in an annular shape to form an assembled structure.
An all-blade steam gas turbine integrated engine characterized by the above. 【請求項６】 摩擦ポンプ（９７）兼用の磁気摩擦動力
伝達装置（１４）により互いに反対方向に回転する外側
軸装置と内側軸装置を最適回転比で結合し、撥水性ター
ビン翼を具備した全動翼ガスタービンの全動翼圧縮機に
おいて、環状に一体鋳造（８４）して組立構造とした夫
々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）としたことを特徴とする全動翼蒸気ガスタービ
ン合体機関。6. An outer shaft device and an inner shaft device, which rotate in mutually opposite directions, are connected at an optimum rotation ratio by a magnetic friction power transmission device (14) which also serves as a friction pump (97), and is equipped with a water repellent turbine blade. A full rotor compressor of a rotor gas turbine is characterized in that an outer compressor rotor blade group (16) and an inner compressor rotor blade group (17) are integrally cast (84) in an annular shape into an assembled structure. Combined full-blade steam gas turbine engine. 【請求項７】 摩擦ポンプ（９７）兼用の磁気摩擦動力
伝達装置（１４）により互いに反対方向に回転する外側
軸装置と内側軸装置を最適回転比で結合し、撥水性ター
ビン翼を具備した全動翼蒸気ガスタービンの全動翼圧縮
機において、環状に一体鋳造（８４）して組立構造とし
た夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼
群（１７）としたことを特徴とする全動翼蒸気ガスター
ビン合体機関。7. A magnetic repulsive power transmission device (14) which also functions as a friction pump (97) connects an outer shaft device and an inner shaft device rotating in opposite directions to each other at an optimum rotation ratio, and is equipped with a water repellent turbine blade. In a full-blade compressor for a moving-blade steam gas turbine, the outer-compressor-blade group (16) and the inner-compressor-blade group (17) are integrally cast (84) in an annular shape to form an assembled structure. Combined full-blade steam gas turbine engine. 【請求項８】 摩擦ポンプ（９７）兼用の磁気摩擦動力
伝達装置（１４）により互いに反対方向に回転する外側
軸装置と内側軸装置を最適回転比で結合し、撥水性ター
ビン翼を具備した全動翼ガスタービンの全動翼圧縮機に
おいて、環状に一体鋳造（８４）して組立構造とした夫
々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）の大部分に、撥水性水冷却翼（８７）を設けた
ことを特徴とする全動翼蒸気ガスタービン合体機関。8. A magnetic friction power transmission device (14) which also functions as a friction pump (97) is used to connect an outer shaft device and an inner shaft device rotating in opposite directions to each other at an optimum rotation ratio to provide a water repellent turbine blade. In the full-blade compressor of a moving-blade gas turbine, most of the outer-compressor-blade group (16) and the inner-compressor-blade group (17) which are integrally cast (84) in an annular shape and have an assembled structure have An all-moving blade steam gas turbine integrated engine having an aqueous water cooling blade (87). 【請求項９】 摩擦ポンプ（９７）兼用の磁気摩擦動力
伝達装置（１４）により互いに反対方向に回転する外側
軸装置と内側軸装置を最適回転比で結合し、撥水性ター
ビン翼を具備した全動翼蒸気ガスタービンの全動翼圧縮
機において、環状に一体鋳造（８４）して組立構造とし
た夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼
群（１７）の大部分に、撥水性水冷却翼（８７）を設け
たことを特徴とする全動翼蒸気ガスタービン合体機関。9. A magnetic friction power transmission device (14) which also serves as a friction pump (97) connects an outer shaft device and an inner shaft device which rotate in opposite directions to each other at an optimum rotation ratio, and is equipped with a water repellent turbine blade. In the full-blade compressor of the bucket steam gas turbine, most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast (84) in an annular shape and have an assembled structure, An all-moving blade steam gas turbine integrated engine having a water-repellent water cooling blade (87). 【請求項１０】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンの全動翼圧
縮機において、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を設
けたことを特徴とする全動翼蒸気ガスタービン合体機
関。10. A full-blade compressor of a full-blade gas turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, A water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) that are integrally cast (84) into an assembled structure. Combined full-blade steam gas turbine engine. 【請求項１１】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの全動
翼圧縮機において、環状に一体鋳造（８４）して組立構
造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮
機動翼群（１７）の大部分に、撥水性水冷却翼（８７）
を設けたことを特徴とする全動翼蒸気ガスタービン合体
機関。11. A full-blade compressor for a full-blade steam gas turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device that rotate in opposite directions by a generator are connected at an optimum rotation ratio, Most of the outer compressor blade group (16) and the inner compressor blade group (17) each having an assembled structure by integrally casting (84) in a ring shape have a water-repellent water cooling blade (87).
An all-blade steam gas turbine combined engine characterized by being provided with. 【請求項１２】 撥水性タービン翼を具備した全動翼ガ
スタービンの全動翼圧縮機において、環状に一体鋳造
（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けたことを特徴
とする全動翼蒸気ガスタービン合体機関。12. A full-blade compressor for a full-blade gas turbine equipped with a water-repellent turbine blade, wherein each outer-compressor blade group (16) and inner side are integrally cast (84) in an annular shape to form an assembled structure. A full-rotor blade steam gas turbine integrated engine, characterized in that a water-repellent water cooling blade (87) is provided in an annular shape for each paragraph in most of the compressor blade group (17). 【請求項１３】 撥水性タービン翼を具備した全動翼蒸
気ガスタービンの全動翼圧縮機において、環状に一体鋳
造（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けたことを特徴
とする全動翼蒸気ガスタービン合体機関。13. A full-blade compressor for a full-blade steam gas turbine equipped with a water-repellent turbine blade, wherein each outer-compressor blade group (16) and an outer-compressor blade group (16) are integrally cast in an annular shape (84) to form an assembled structure. A total moving blade steam gas turbine combined engine, wherein a water repellent water cooling blade (87) is provided in an annular shape for each paragraph in most of the inner compressor blade group (17). 【請求項１４】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼ガスタービンの全動翼圧縮機
において、環状に一体鋳造（８４）して組立構造とした
夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）の大部分に、撥水性水冷却翼（８７）を段落毎
環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷
却後に水噴射手段（５６）より水噴射することを特徴と
する全動翼蒸気ガスタービン合体機関。14. A magnetic friction power transmission device (14) which also serves as a friction pump (97) is used to couple an outer shaft device and an inner shaft device rotating in opposite directions with each other at an optimum rotation ratio to provide a water repellent turbine blade. In the full-blade compressor of a moving-blade gas turbine, most of the outer-compressor-blade group (16) and the inner-compressor-blade group (17) which are integrally cast (84) in an annular shape and have an assembled structure have An all-blade steam gas turbine characterized in that an aqueous water cooling blade (87) is provided in an annular shape for each paragraph, and water is injected from a water injection means (56) after cooling one or more water-repellent water cooling blades for each paragraph. Coalescing agency. 【請求項１５】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼蒸気ガスタービンの全動翼圧
縮機において、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼
を冷却後に水噴射手段（５６）より水噴射することを特
徴とする全動翼蒸気ガスタービン合体機関。15. A magnetic friction power transmission device (14) which also serves as a friction pump (97) is used to couple an outer shaft device and an inner shaft device rotating in opposite directions to each other at an optimum rotation ratio, and a water repellent turbine blade is provided. In the full-blade compressor of the bucket steam gas turbine, most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast (84) in an annular shape and have an assembled structure, Water-repellent water cooling blade (87) is provided in an annular shape for each paragraph, and one or more water-repellent water cooling blades for each paragraph are cooled and then water-injected by water injection means (56). Turbine united engine. 【請求項１６】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンの全動翼圧
縮機において、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼
を冷却後に水噴射手段（５６）より水噴射することを特
徴とする全動翼蒸気ガスタービン合体機関。16. A full-blade compressor for a full-blade gas turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, Most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast (84) into an assembled structure, are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph. In addition, the water-injection means (56) injects water after cooling one or more water-repellent water-cooling blades per paragraph. 【請求項１７】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの全動
翼圧縮機において、環状に一体鋳造（８４）して組立構
造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮
機動翼群（１７）の大部分に、撥水性水冷却翼（８７）
を段落毎環状に設けて、段落毎１以上複数の撥水性水冷
却翼を冷却後に水噴射手段（５６）より水噴射すること
を特徴とする全動翼蒸気ガスタービン合体機関。17. A full-blade compressor for a full-blade steam gas turbine equipped with a water-repellent turbine blade, in which an outer shaft device and an inner shaft device that rotate in opposite directions by a generator are connected at an optimum rotation ratio, Most of the outer compressor blade group (16) and the inner compressor blade group (17) each having an assembled structure by integrally casting (84) in a ring shape have a water-repellent water cooling blade (87).
Is provided in an annular shape for each paragraph, and water is injected from a water injection means (56) after cooling one or more water-repellent water cooling blades for each paragraph. 【請求項１８】 撥水性タービン翼を具備した全動翼ガ
スタービンの全動翼圧縮機において、環状に一体鋳造
（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けて、段落毎１
以上複数の撥水性水冷却翼を冷却後に水噴射手段（５
６）より水噴射することを特徴とする全動翼蒸気ガスタ
ービン合体機関。18. A full-blade compressor for a full-blade gas turbine equipped with water-repellent turbine blades, wherein each outer-compressor blade group (16) and inner side are integrally cast (84) to form an assembled structure. A water-repellent water cooling blade (87) is provided in an annular shape for each paragraph on most of the compressor blade group (17).
After cooling the plurality of water-repellent water cooling blades, the water jetting means (5
6) A full-blade steam gas turbine integrated engine characterized by water injection from 【請求項１９】 撥水性タービン翼を具備した全動翼蒸
気ガスタービンの全動翼圧縮機において、環状に一体鋳
造（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けて、段落毎１
以上複数の撥水性水冷却翼を冷却後に水噴射手段（５
６）より水噴射することを特徴とする全動翼蒸気ガスタ
ービン合体機関。19. A full-blade compressor for a full-blade steam gas turbine equipped with a water-repellent turbine blade, wherein each outer-compressor blade group (16) and an outer-compressor blade group (16) are integrally cast (84) in an annular shape to form an assembled structure. A water-repellent water cooling blade (87) is provided in an annular shape for each paragraph in most of the inner compressor rotor blade group (17).
After cooling the plurality of water-repellent water cooling blades, the water jetting means (5
6) A full-blade steam gas turbine integrated engine characterized by water injection from 【請求項２０】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼ガスタービンの全動翼圧縮機
において、環状に一体鋳造（８４）して組立構造とした
夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）の大部分に、撥水性水冷却翼（８７）を段落毎
環状に設けて、段落毎全部以下半分の撥水性水冷却翼を
冷却後に水噴射手段（５６）より水噴射することを特徴
とする全動翼蒸気ガスタービン合体機関。20. A magnetic friction power transmission device (14) which also serves as a friction pump (97) connects an outer shaft device and an inner shaft device, which rotate in mutually opposite directions, at an optimum rotation ratio, and is equipped with a water repellent turbine blade. In the full-blade compressor of a moving-blade gas turbine, most of the outer-compressor-blade group (16) and the inner-compressor-blade group (17) which are integrally cast (84) in an annular shape and have an assembled structure have An all-blade steam gas turbine characterized in that an aqueous water cooling blade (87) is provided in an annular shape for each paragraph, and water is injected from a water injection means (56) after cooling all or less of the water-repellent water cooling blades for each paragraph. Coalescing agency. 【請求項２１】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼蒸気ガスタービンの全動翼圧
縮機において、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて、段落毎全部以下半分の撥水性水冷却
翼を冷却後に水噴射手段（５６）より水噴射することを
特徴とする全動翼蒸気ガスタービン合体機関。21. A magnetic friction power transmission device (14) which also serves as a friction pump (97) is used to couple an outer shaft device and an inner shaft device rotating in mutually opposite directions at an optimum rotation ratio, and a water repellent turbine blade is provided. In the full-blade compressor of a rotor-blade gas turbine, most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are integrally cast (84) in an annular shape to have an assembled structure. A water vapor repellent water cooling blade (87) is provided in an annular shape for each paragraph, and water is injected from a water injection means (56) after cooling all or less of the water repellent water cooling blades for each paragraph. Turbine united engine. 【請求項２２】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンの全動翼圧
縮機において、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて、段落毎全部以下半分の撥水性水冷却
翼を冷却後に水噴射手段（５６）より水噴射することを
特徴とする全動翼蒸気ガスタービン合体機関。22. A full-blade compressor for a full-blade gas turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, Most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast (84) into an assembled structure, are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph. And a water-injection means (56) for injecting water after cooling all or less than half of the water-repellent water cooling blades for each paragraph. 【請求項２３】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの全動
翼圧縮機において、環状に一体鋳造（８４）して組立構
造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮
機動翼群（１７）の大部分に、撥水性水冷却翼（８７）
を段落毎環状に設けて、段落毎全部以下半分の撥水性水
冷却翼を冷却後に水噴射手段（５６）より水噴射するこ
とを特徴とする全動翼蒸気ガスタービン合体機関。23. An all-blade compressor for a full-blade steam gas turbine comprising a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device that rotate in opposite directions by a generator are combined at an optimum rotation ratio. Most of the outer compressor blade group (16) and the inner compressor blade group (17) each having an assembled structure by integrally casting (84) in a ring shape have a water-repellent water cooling blade (87).
Is provided in an annular shape for each paragraph, and water is injected from the water injection means (56) after cooling all or less of the water-repellent water cooling blades for all the paragraphs. 【請求項２４】 撥水性タービン翼を具備した全動翼ガ
スタービンの全動翼圧縮機において、環状に一体鋳造
（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けて、段落毎全
部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５
６）より水噴射することを特徴とする全動翼蒸気ガスタ
ービン合体機関。24. A full-blade compressor for a full-blade gas turbine equipped with a water-repellent turbine blade, wherein each outer-compressor blade group (16) and inner side are integrally cast (84) to form an assembled structure. A water-repellent water cooling blade (87) is provided in an annular shape for each paragraph on most of the compressor blade group (17), and after the water-repellent water cooling blade is cooled to half or less for each paragraph, water injection means (5) is used.
6) A full-blade steam gas turbine integrated engine characterized by water injection from 【請求項２５】 撥水性タービン翼を具備した全動翼蒸
気ガスタービンの全動翼圧縮機において、環状に一体鋳
造（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けて、段落毎全
部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５
６）より水噴射することを特徴とする全動翼蒸気ガスタ
ービン合体機関。25. In an all-blade compressor of an all-blade steam gas turbine equipped with a water-repellent turbine blade, an outer compressor blade group (16) and an outer-compressor blade group (16) which are integrally cast in an annular shape (84) and have an assembled structure A water-repellent water cooling blade (87) is provided in an annular shape for each paragraph in most of the inner compressor rotor blade group (17), and after the water-repellent water cooling blade is cooled to half or less for each paragraph, water injection means (5) is used.
6) A full-blade steam gas turbine integrated engine characterized by water injection from 【請求項２６】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼ガスタービンにおいて、環状
に一体鋳造（８４）して組立構造として水路を連通した
夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）の大部分に、撥水性水冷却翼（８７）を段落毎
環状に設けて、段落毎全部以下半分の撥水性水冷却翼を
冷却後に水噴射手段（５６）より水噴射することを特徴
とする全動翼蒸気ガスタービン合体機関。26. A magnetic friction power transmission device (14) which also serves as a friction pump (97) connects an outer shaft device and an inner shaft device that rotate in opposite directions to each other at an optimum rotation ratio, and has a water repellent turbine blade. In a rotor blade gas turbine, water-repellent water cooling is applied to most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are integrally cast (84) in an annular shape and communicate with the water passage as an assembled structure. An all-blade steam-gas turbine integrated engine, characterized in that the blades (87) are annularly provided for each paragraph, and water is injected from the water injection means (56) after cooling all or less of the water-repellent water cooling vanes for each paragraph. 【請求項２７】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼蒸気ガスタービンにおいて、
環状に一体鋳造（８４）して組立構造として水路を連通
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて、段落毎全部以下半分の撥水性水冷却
翼を冷却後に水噴射手段（５６）より水噴射することを
特徴とする全動翼蒸気ガスタービン合体機関。27. A magnetic frictional power transmission device (14) which also serves as a friction pump (97) connects an outer shaft device and an inner shaft device which rotate in opposite directions to each other at an optimum rotation ratio, and comprises a water repellent turbine blade. In a blade steam gas turbine,
A water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast in an annular shape (84) and communicate with each other as an assembled structure. A full moving blade steam gas turbine integrated engine, characterized in that the water repellent water cooling blades, which are provided in each annular shape and are less than half each of the paragraphs, are water-injected by a water injection means (56) after cooling. 【請求項２８】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンにおいて、
環状に一体鋳造（８４）して組立構造として水路を連通
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて、段落毎全部以下半分の撥水性水冷却
翼を冷却後に水噴射手段（５６）より水噴射することを
特徴とする全動翼蒸気ガスタービン合体機関。28. A full-blade gas turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device that rotate in opposite directions by a generator are combined at an optimum rotation ratio,
A water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast in an annular shape (84) and communicate with each other as an assembled structure. A full moving blade steam gas turbine integrated engine, characterized in that the water repellent water cooling blades, which are provided in each annular shape and are less than half each of the paragraphs, are water-injected by a water injection means (56) after cooling. 【請求項２９】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンにおい
て、環状に一体鋳造（８４）して組立構造として水路を
連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮
機動翼群（１７）の大部分に、撥水性水冷却翼（８７）
を段落毎環状に設けて、段落毎全部以下半分の撥水性水
冷却翼を冷却後に水噴射手段（５６）より水噴射するこ
とを特徴とする全動翼蒸気ガスタービン合体機関。29. In an all-blade steam gas turbine equipped with a water repellent turbine blade, an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, and are integrally cast in an annular shape (84). ), The water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) that communicate with the water channel as an assembled structure.
Is provided in an annular shape for each paragraph, and water is injected from the water injection means (56) after cooling all or less of the water-repellent water cooling blades for all the paragraphs. 【請求項３０】 撥水性タービン翼を具備した全動翼ガ
スタービンにおいて、環状に一体鋳造（８４）して組立
構造として水路を連通した夫々の外側圧縮機動翼群（１
６）及び内側圧縮機動翼群（１７）の大部分に、撥水性
水冷却翼（８７）を段落毎環状に設けて、段落毎全部以
下半分の撥水性水冷却翼を冷却後に水噴射手段（５６）
より水噴射することを特徴とする全動翼蒸気ガスタービ
ン合体機関。30. In an all-blade gas turbine equipped with a water-repellent turbine blade, each outer compressor rotor blade group (1) is integrally cast in an annular shape (84) and communicates with a water channel as an assembly structure.
6) and most of the inner compressor rotor blade group (17), a water-repellent water cooling blade (87) is provided in an annular shape for each paragraph, and water cooling means ( 56)
A full-blade steam gas turbine combined engine characterized by more water injection. 【請求項３１】 撥水性タービン翼を具備した全動翼蒸
気ガスタービンにおいて、環状に一体鋳造（８４）して
組立構造として水路を連通した夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けて、段落毎全
部以下半分の撥水性水冷却翼を冷却後に水噴射手段（５
６）より水噴射することを特徴とする全動翼蒸気ガスタ
ービン合体機関。31. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, an outer compressor rotor blade group (16) and an inner compressor rotor which are integrally cast in an annular shape (84) and have water channels communicating as an assembly structure. A water-repellent water cooling blade (87) is annularly provided in each of the paragraphs on most of the blade group (17), and after each half of the water-repellent water cooling blades are cooled, water injection means (5) is provided.
6) A full-blade steam gas turbine integrated engine characterized by water injection from 【請求項３２】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼ガスタービンの全動翼圧縮機
において、環状に一体鋳造（８４）して組立構造とした
夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）の大部分に、撥水性水冷却翼（８７）を段落毎
環状に設けて該出力で駆動する装置を具備したことを特
徴とする全動翼蒸気ガスタービン合体機関。32. An outer shaft device and an inner shaft device, which rotate in mutually opposite directions, are coupled at an optimum rotation ratio by a magnetic friction power transmission device (14) which also serves as a friction pump (97), and a water-repellent turbine blade is provided as a whole. In the full-blade compressor of a moving-blade gas turbine, most of the outer-compressor-blade group (16) and the inner-compressor-blade group (17) which are integrally cast (84) in an annular shape and have an assembled structure have An all-blade steam-gas turbine integrated engine, characterized in that an aqueous water cooling vane (87) is provided in an annular shape for each paragraph and is equipped with a device driven by the output. 【請求項３３】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼蒸気ガスタービンの全動翼圧
縮機において、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて該出力で駆動する装置を具備したこと
を特徴とする全動翼蒸気ガスタービン合体機関。33. A magnetic frictional power transmission device (14) which also serves as a friction pump (97) connects an outer shaft device and an inner shaft device, which rotate in mutually opposite directions, at an optimum rotation ratio, and is provided with a water repellent turbine blade. In the full-blade compressor of the bucket steam gas turbine, most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast (84) in an annular shape and have an assembled structure, A total moving blade steam gas turbine integrated engine, comprising: a water repellent water cooling blade (87) provided in an annular shape for each paragraph and equipped with a device driven by the output. 【請求項３４】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンの全動翼圧
縮機において、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて該出力で駆動する装置を具備したこと
を特徴とする全動翼蒸気ガスタービン合体機関。34. A full-blade compressor for a full-blade gas turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are connected at an optimum rotation ratio, Most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast (84) into an assembled structure, are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph. And a device driven by the output. 【請求項３５】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの全動
翼圧縮機において、環状に一体鋳造（８４）して組立構
造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮
機動翼群（１７）の大部分に、撥水性水冷却翼（８７）
を段落毎環状に設けて該出力で駆動する装置を具備した
ことを特徴とする全動翼蒸気ガスタービン合体機関。35. A full-blade compressor for a full-blade steam gas turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device that rotate in opposite directions by a generator are combined at an optimum rotation ratio, Most of the outer compressor blade group (16) and the inner compressor blade group (17) each having an assembled structure by integrally casting (84) in a ring shape have a water-repellent water cooling blade (87).
Is provided in an annular shape for each paragraph and is equipped with a device that is driven by the output. 【請求項３６】 撥水性タービン翼を具備した全動翼ガ
スタービンの全動翼圧縮機において、環状に一体鋳造
（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けて該出力で駆
動する装置を具備したことを特徴とする全動翼蒸気ガス
タービン合体機関。36. A full-blade compressor for a full-blade gas turbine having water-repellent turbine blades, wherein each outer-compressor blade group (16) and inner side are integrally cast (84) into an assembled structure to form an assembled structure. A full-rotor blade steam gas turbine integrated engine, characterized in that a water-repellent water cooling blade (87) is provided in an annular shape for each paragraph in a majority of the compressor blade group (17) and is driven by the output. 【請求項３７】 撥水性タービン翼を具備した全動翼蒸
気ガスタービンの全動翼圧縮機において、環状に一体鋳
造（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けて該出力で駆
動する装置を具備したことを特徴とする全動翼蒸気ガス
タービン合体機関。37. A full-blade compressor for a full-blade steam gas turbine equipped with a water-repellent turbine blade, wherein each outer-compressor blade group (16) and an outer-compressor blade group (16) are integrally cast into an annular shape (84) to form an assembled structure. A full-blade steam-gas turbine integrated engine, characterized in that a water-repellent water cooling blade (87) is provided in an annular shape for each paragraph in a majority of the inner compressor blade group (17) and is driven by the output. . 【請求項３８】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼ガスタービンの全動翼圧縮機
において、環状に一体鋳造（８４）して組立構造とした
夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）の大部分に、撥水性水冷却翼（８７）を段落毎
環状に設けて、段落毎１以上複数の撥水性水冷却翼を冷
却後に水噴射手段（５６）より水噴射して該出力で駆動
する装置を具備したことを特徴とする全動翼蒸気ガスタ
ービン合体機関。38. A magnetic friction power transmission device (14) which also serves as a friction pump (97) connects an outer shaft device and an inner shaft device, which rotate in mutually opposite directions, at an optimum rotation ratio, and is equipped with a water repellent turbine blade. In the full-blade compressor of a moving-blade gas turbine, most of the outer-compressor-blade group (16) and the inner-compressor-blade group (17) which are integrally cast (84) in an annular shape and have an assembled structure have An aqueous water cooling vane (87) is provided in an annular shape for each paragraph, and one or more water repellent water cooling vanes for each paragraph are cooled, and then water jetting means (56) jets water to drive with the output. An all-blade steam gas turbine integrated engine characterized by. 【請求項３９】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼蒸気ガスタービンの全動翼圧
縮機において、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼
を冷却後に水噴射手段（５６）より水噴射して該出力で
駆動する装置を具備したことを特徴とする全動翼蒸気ガ
スタービン合体機関。39. A magnetic friction power transmission device (14) also serving as a friction pump (97) is used to couple an outer shaft device and an inner shaft device rotating in mutually opposite directions at an optimum rotation ratio, and a water repellent turbine blade is provided. In the full-blade compressor of a rotor-blade gas turbine, most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17) are integrally cast (84) in an annular shape to have an assembled structure. A water-repellent water cooling blade (87) was provided in an annular shape for each paragraph, and a device for injecting water from water injection means (56) after cooling one or more water-repellent water cooling blades for each paragraph and driving with the output was provided. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項４０】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンの全動翼圧
縮機において、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて、段落毎１以上複数の撥水性水冷却翼
を冷却後に水噴射手段（５６）より水噴射して該出力で
駆動する装置を具備したことを特徴とする全動翼蒸気ガ
スタービン合体機関。40. A full-blade compressor for a full-blade gas turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device that rotate in opposite directions by a generator are connected at an optimum rotation ratio, Most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast (84) into an assembled structure, are provided with water-repellent water cooling blades (87) in an annular shape for each paragraph. An all-blade steam-gas turbine integrated engine comprising a device for injecting water from a water injecting means (56) after cooling one or more water-repellent water cooling blades per paragraph and driving with the output. 【請求項４１】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの全動
翼圧縮機において、環状に一体鋳造（８４）して組立構
造とした夫々の外側圧縮機動翼群（１６）及び内側圧縮
機動翼群（１７）の大部分に、撥水性水冷却翼（８７）
を段落毎環状に設けて、段落毎１以上複数の撥水性水冷
却翼を冷却後に水噴射手段（５６）より水噴射して該出
力で駆動する装置を具備したことを特徴とする全動翼蒸
気ガスタービン合体機関。41. A full-blade compressor for a full-blade steam gas turbine equipped with a water-repellent turbine blade, in which an outer shaft device and an inner shaft device that rotate in opposite directions by a generator are connected at an optimum rotation ratio, Most of the outer compressor blade group (16) and the inner compressor blade group (17) each having an assembled structure by integrally casting (84) in a ring shape have a water-repellent water cooling blade (87).
Is provided in an annular shape for each paragraph, and after the plurality of water-repellent water cooling blades for each paragraph are cooled, a device for injecting water from a water injection means (56) and driving with the output is provided. Steam gas turbine integrated engine. 【請求項４２】 撥水性タービン翼を具備した全動翼ガ
スタービンの全動翼圧縮機において、環状に一体鋳造
（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けて、段落毎１
以上複数の撥水性水冷却翼を冷却後に水噴射手段（５
６）より水噴射して該出力で駆動する装置を具備したこ
とを特徴とする全動翼蒸気ガスタービン合体機関。42. A full-blade compressor for a full-blade gas turbine equipped with water-repellent turbine blades, wherein each outer-compressor blade group (16) and inner side are integrally cast (84) into an assembly structure. A water-repellent water cooling blade (87) is provided in an annular shape for each paragraph on most of the compressor blade group (17), and each paragraph is
After cooling the plurality of water-repellent water cooling blades, the water jetting means (5
6) An all-blade steam gas turbine united engine equipped with a device for injecting water from 6) and driving with the output. 【請求項４３】 撥水性タービン翼を具備した全動翼蒸
気ガスタービンの全動翼圧縮機において、環状に一体鋳
造（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けて、段落毎１
以上複数の撥水性水冷却翼を冷却後に水噴射手段（５
６）より水噴射し該出力で駆動する装置を具備したこと
を特徴とする全動翼蒸気ガスタービン合体機関。43. A full-blade compressor for a full-blade steam gas turbine equipped with water-repellent turbine blades, wherein each outer-compressor blade group (16) and an outer-compressor blade group (16) are integrally cast in an annular shape (84) into an assembled structure. A water-repellent water cooling blade (87) is provided in an annular shape for each paragraph on most of the inner compressor rotor blade group (17).
After cooling the plurality of water-repellent water cooling blades, the water jetting means (5
6) An all-blade steam gas turbine integrated engine equipped with a device for injecting water according to 6) and driving with the output. 【請求項４４】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼ガスタービンにおいて、環状
に一体鋳造（８４）して組立構造として水路を連通した
夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）の大部分に、撥水性水冷却翼（８７）を段落毎
環状に設けて、段落毎全部以下半分の撥水性水冷却翼を
冷却後に水噴射手段（５６）より水噴射して該出力で駆
動する装置を具備したことを特徴とする全動翼蒸気ガス
タービン合体機関。44. A magnetic friction power transmission device (14) which also serves as a friction pump (97) connects an outer shaft device and an inner shaft device that rotate in opposite directions to each other at an optimum rotation ratio, and is equipped with a water repellent turbine blade. In a rotor blade gas turbine, water-repellent water cooling is applied to most of the outer compressor rotor blade group (16) and the inner compressor rotor blade group (17), which are integrally cast (84) in an annular shape and communicate with the water passage as an assembled structure. A blade (87) is provided in an annular shape for each paragraph, and a device for injecting water from the water injection means (56) after cooling half or less water-repellent water cooling blades for each paragraph and driving with the output is provided. Combined full-blade steam gas turbine engine. 【請求項４５】 摩擦ポンプ（９７）兼用の磁気摩擦動
力伝達装置（１４）により互いに反対方向に回転する外
側軸装置と内側軸装置を最適回転比で結合し、撥水性タ
ービン翼を具備した全動翼蒸気ガスタービンにおいて、
環状に一体鋳造（８４）して組立構造として水路を連通
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて、段落毎全部以下半分の撥水性水冷却
翼を冷却後に水噴射手段（５６）より水噴射して該出力
で駆動する装置を具備したことを特徴とする全動翼蒸気
ガスタービン合体機関。45. A magnetic friction power transmission device (14) which also serves as a friction pump (97) connects an outer shaft device and an inner shaft device that rotate in opposite directions to each other at an optimum rotation ratio, and has a water repellent turbine blade. In a blade steam gas turbine,
A water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast in an annular shape (84) and communicate with each other as an assembled structure. All moving blade steam gas, characterized in that it is provided with an annular shape, and comprises a device for cooling less than half of the water-repellent water cooling blades for each paragraph, and then injecting water from a water injection means (56) and driving with this output. Turbine united engine. 【請求項４６】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンにおいて、
環状に一体鋳造（８４）して組立構造として水路を連通
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて、段落毎全部以下半分の撥水性水冷却
翼を冷却後に水噴射手段（５６）より水噴射して該出力
で駆動する装置を具備したことを特徴とする全動翼蒸気
ガスタービン合体機関。46. An all-blade gas turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device that rotate in mutually opposite directions by a generator are combined at an optimum rotation ratio,
A water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally cast in an annular shape (84) and communicate with each other as an assembled structure. All moving blade steam gas, characterized in that it is provided with an annular shape, and comprises a device for cooling less than half of the water-repellent water cooling blades for each paragraph, and then injecting water from a water injection means (56) and driving with this output. Turbine united engine. 【請求項４７】 発電機により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンにおい
て、環状に一体鋳造（８４）して組立構造として水路を
連通した夫々の外側圧縮機動翼群（１６）及び内側圧縮
機動翼群（１７）の大部分に、撥水性水冷却翼（８７）
を段落毎環状に設けて、段落毎全部以下半分の撥水性水
冷却翼を冷却後に水噴射手段（５６）より水噴射して該
出力で駆動する装置を具備したことを特徴とする全動翼
蒸気ガスタービン合体機関。47. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, and are integrally cast in an annular shape (84). ), The water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) that communicate with the water channel as an assembled structure.
Is provided in an annular shape for each paragraph, and a water-repellent water cooling blade that is half or less than all the paragraphs is cooled, and thereafter water jetting means (56) jets water to drive with the output. Steam gas turbine integrated engine. 【請求項４８】 撥水性タービン翼を具備した全動翼ガ
スタービンにおいて、環状に一体鋳造（８４）して組立
構造として水路を連通した夫々の外側圧縮機翼群及び内
側圧縮機動翼群（１７）の大部分に、撥水性水冷却翼
（８７）を段落毎環状に設けて、段落毎全部以下半分の
撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴
射して該出力で駆動する装置を具備したことを特徴とす
る全動翼蒸気ガスタービン合体機関。48. In an all-blade gas turbine equipped with water-repellent turbine blades, an outer compressor blade group and an inner compressor blade group (17) which are integrally cast in an annular shape (84) and have water channels communicating as an assembled structure. ), A water-repellent water cooling blade (87) is provided in an annular shape for each paragraph, and after cooling half or less of all water-repellent water cooling blades for each paragraph, water is jetted from the water jetting means (56) to produce the output. An all-blade steam gas turbine integrated engine having a driving device. 【請求項４９】 撥水性タービン翼を具備した全動翼蒸
気ガスタービンにおいて、環状に一体鋳造（８４）して
組立構造として水路を連通した夫々の外側圧縮機翼群及
び内側圧縮機動翼群（１７）の大部分に、撥水性水冷却
翼（８７）を段落毎環状に設けて、段落毎全部以下半分
の撥水性水冷却翼を冷却後に水噴射手段（５６）より水
噴射して該出力で駆動する装置を具備したことを特徴と
する全動翼蒸気ガスタービン合体機関。49. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, an outer compressor blade group and an inner compressor blade group which are integrally cast (84) in an annular shape and have water channels communicating as an assembly structure ( The water-repellent water cooling blade (87) is provided in an annular shape for each paragraph in most of (17), and water is injected from the water-injection means (56) after cooling all the water-repellent water cooling blades of half or less for each paragraph and the output. An all-blade steam gas turbine integrated engine, characterized in that it is equipped with a device driven by. 【請求項５０】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼ガスタービン
において、極低温燃焼ガスを核に水や水蒸気を凝集し
て、雹や水滴等として分別回収可能にすることを特徴と
する全動翼蒸気ガスタービン合体機関。50. A full-blade gas turbine equipped with a water-repellent turbine blade, which brings a combustion gas exhaust gas temperature close to −273 ° C., aggregates water or steam by using a cryogenic combustion gas as a nucleus to form hail or water droplets. An all-blade steam gas turbine integrated engine characterized by enabling separate collection. 【請求項５１】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼ガスタービン
において、石炭灰を含む極低温燃焼ガスを核に水や水蒸
気を凝集して、雹や水滴等として分別回収可能にするこ
とを特徴とする全動翼蒸気ガスタービン合体機関。51. In an all-blade gas turbine equipped with a water repellent turbine blade, which brings a combustion gas exhaust gas temperature close to -273 ° C., water and steam are condensed by using a cryogenic combustion gas containing coal ash as a core to form a hail. An all-blade steam gas turbine integrated engine characterized by enabling separate collection as water droplets, etc. 【請求項５２】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼ガスタービン
において、有害物質を含む極低温燃焼ガスを核に水や水
蒸気を凝集して、雹や水滴等として分別回収可能にする
ことを特徴とする全動翼蒸気ガスタービン合体機関。52. In an all-blade gas turbine equipped with a water-repellent turbine blade, which brings a combustion gas exhaust gas temperature close to -273 ° C., water or steam is condensed by using a cryogenic combustion gas containing a harmful substance as a core to form a hail. An all-blade steam gas turbine integrated engine characterized by enabling separate collection as water droplets, etc. 【請求項５３】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼蒸気ガスター
ビンにおいて、極低温燃焼ガスを核に水や水蒸気を凝集
し、雹や水滴等として分別回収可能にすることを特徴と
する全動翼蒸気ガスタービン合体機関。53. In a full-blade steam gas turbine equipped with a water repellent turbine blade, which brings a combustion gas exhaust gas temperature close to -273 ° C., water or steam is condensed as a hail or a water drop etc. by using a cryogenic combustion gas as a core. An all-blade steam gas turbine combined engine characterized by enabling separate collection. 【請求項５４】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼蒸気ガスター
ビンにおいて、石炭灰を含む極低温燃焼ガスを核に水や
水蒸気を凝集して、雹や水滴等として分別回収可能にす
ることを特徴とする全動翼蒸気ガスタービン合体機関。54. In a full-blade steam gas turbine equipped with a water-repellent turbine blade, which brings a combustion gas exhaust gas temperature close to -273 ° C., by coagulating water or steam with a cryogenic combustion gas containing coal ash as a core, An all-blade steam gas turbine integrated engine characterized by enabling separate collection as hail and water droplets. 【請求項５５】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備し全動翼蒸気ガスタービ
ンにおいて、有害物質を含む極低温燃焼ガスを核に水や
水蒸気を凝集して、雹や水滴等として分別回収可能にす
ることを特徴とする全動翼蒸気ガスタービン合体機関。55. In an all-blade steam gas turbine equipped with a water-repellent turbine blade for bringing a combustion gas exhaust gas temperature close to −273 ° C., water or steam is condensed with a cryogenic combustion gas containing a harmful substance as a core, An all-blade steam gas turbine united engine that enables separate collection as hail and water droplets. 【請求項５６】 燃焼ガス排気温度を−２７３℃に近付
ける、摩擦ポンプ（９７）兼用の、磁気摩擦動力伝達装
置（１４）により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼ガスタービンにおいて、極低温燃焼ガ
スを核に水や水蒸気を凝集して、雹や水滴等として分別
回収可能にすることを特徴とする全動翼蒸気ガスタービ
ン合体機関。56. An optimum rotation ratio between an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also functions as a friction pump (97) and that makes a combustion gas exhaust gas temperature close to −273 ° C. In an all-blade gas turbine equipped with a water-repellent turbine blade, the total operation is characterized by coagulating water and water vapor with a cryogenic combustion gas as a core to enable separate collection as hail and water droplets. Wing steam gas turbine combined engine. 【請求項５７】 燃焼ガス排気温度を−２７３℃に近付
ける、摩擦ポンプ（９７）兼用の、磁気摩擦動力伝達装
置（１４）により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼ガスタービンにおいて、有害物質を含
む極低温燃焼ガスを核に水や水蒸気を凝集して、雹や水
滴等として分別回収可能にすることを特徴とする全動翼
蒸気ガスタービン合体機関。57. An optimum rotation ratio of an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also functions as a friction pump (97) and that brings a combustion gas exhaust gas temperature close to -273 ° C. In an all-blade gas turbine equipped with water-repellent turbine blades, water and water vapor are aggregated in the core of cryogenic combustion gas containing harmful substances to enable separate collection as hail and water droplets. Combined full-blade steam gas turbine engine. 【請求項５８】 燃焼ガス排気温度を−２７３℃に近付
ける、摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼蒸気ガスタービンにおいて、極低温燃焼
ガスを核に水や水蒸気を凝集して、雹や水滴等として分
別回収可能にすることを特徴とする全動翼蒸気ガスター
ビン合体機関。58. An outer shaft device and an inner shaft device, which rotate in opposite directions by a magnetic friction power transmission device (14) which also functions as a friction pump (97), which makes a combustion gas exhaust gas temperature close to −273 ° C., have an optimum rotation ratio. In a full-blade steam gas turbine equipped with a water-repellent turbine blade combined with each other, the full-speed steam gas turbine is characterized by aggregating water and water vapor with a cryogenic combustion gas as a core, and making it possible to separately collect as hail and water droplets. Wing steam gas turbine combined engine. 【請求項５９】 燃焼ガス排気温度を−２７３℃に近付
ける、摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼蒸気ガスタービンにおいて、有害物質を
含む極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収可能にすることを特徴とする全動
翼蒸気ガスタービン合体機関。59. An outer shaft device and an inner shaft device, which rotate in opposite directions by a magnetic friction power transmission device (14) which also functions as a friction pump (97), which makes a combustion gas exhaust gas temperature close to −273 ° C., have an optimum rotation ratio. Combined, in a full-blade steam gas turbine equipped with a water-repellent turbine blade, it is characterized by aggregating water and steam with cryogenic combustion gas containing harmful substances as the core, and making it possible to separate and collect as hail and water droplets. Combined full-blade steam gas turbine engine. 【請求項６０】 燃焼ガス排気温度を−２７３℃に近付
ける、発電機により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼ガスタービンにおいて、極低温燃焼
ガスを核に水や水蒸気を凝集して、雹や水滴等として分
別回収可能にすることを特徴とする蒸気ガスタービン合
体機関。60. A total rotor blade having a water repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are combined at an optimum rotation ratio, and a combustion gas exhaust temperature approaches −273 ° C. In a gas turbine, a steam gas turbine integrated engine, characterized in that water and steam are condensed by using a cryogenic combustion gas as a core, and can be separately collected as hail, water droplets and the like. 【請求項６１】 燃焼ガス排気温度を−２７３℃に近付
ける、発電機により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼ガスタービンにおいて、有害物質を
含む極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収可能にすることを特徴とする全動
翼蒸気ガスタービン合体機関。61. A total rotor blade having a water-repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are combined at an optimum rotation ratio, the combustion gas exhaust gas temperature approaching −273 ° C. In a gas turbine, an all-blade steam gas turbine integrated engine characterized by aggregating water and water vapor with a cryogenic combustion gas containing a harmful substance as a core, and making it possible to separately collect as a hail or a water drop. 【請求項６２】 燃焼ガス排気温度を−２７３℃に近付
ける、発電機により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼蒸気ガスタービンにおいて、極低温
燃焼ガスを核に水や水蒸気を凝集して、雹や水滴等とし
て分別回収可能にすることを特徴とする全動翼蒸気ガス
タービン合体機関。62. A rotor blade having a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are combined at an optimum rotation ratio, and a combustion gas exhaust temperature approaches −273 ° C. In a steam gas turbine, an all-blade steam gas turbine integrated engine characterized by aggregating water and steam with a cryogenic combustion gas as a core to enable separate collection as hail and water droplets. 【請求項６３】 燃焼ガス排気温度を−２７３℃に近付
ける、発電機により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼蒸気ガスタービンにおいて、有害物
質を含む極低温燃焼ガスを核に水や水蒸気を凝集して、
雹や水滴等として分別回収可能にすることを特徴とする
全動翼蒸気ガスタービン合体機関。63. A total rotor blade having a water repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are coupled at an optimum rotation ratio, and a combustion gas exhaust temperature approaches −273 ° C. In a steam gas turbine, a cryogenic combustion gas containing harmful substances is used as a core to aggregate water and steam,
An all-blade steam gas turbine united engine that enables separate collection as hail and water droplets. 【請求項６４】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼ガスタービン
において、環状に一体鋳造（８４）して組立構造とした
夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）の大部分に、水冷却翼（８７）を段落毎環状に
設けたことを特徴とする全動翼蒸気ガスタービン合体機
関。64. In an all-blade gas turbine having a water-repellent turbine blade for bringing a combustion gas exhaust gas temperature close to -273 ° C., each outer compressor blade group having an assembled structure by integrally casting (84) in an annular shape. (16) and a majority of the inner compressor moving blade group (17), a water cooling blade (87) is provided in an annular shape for each paragraph, a full rotor steam gas turbine combined engine. 【請求項６５】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼蒸気ガスター
ビンにおいて、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、水冷却翼（８７）を段落毎環
状に設けたことを特徴とする全動翼蒸気ガスタービン合
体機関。65. In an all-blade steam gas turbine equipped with a water-repellent turbine blade for bringing a combustion gas exhaust gas temperature close to −273 ° C., each outer compressor blade is integrally cast (84) in an annular shape to form an assembled structure. A full-blade steam gas turbine integrated engine, characterized in that a water cooling blade (87) is provided in an annular shape for each paragraph in most of the group (16) and the inner compressor rotor blade group (17). 【請求項６６】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼ガスタービンにおいて、環状に一体鋳造
（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、水
冷却翼（８７）を段落毎環状に設けたことを特徴とする
全動翼蒸気ガスタービン合体機関。66. An outer shaft device and an inner shaft device, which rotate in mutually opposite directions, are combined at an optimum rotation ratio by a magnetic friction power transmission device (14) which also serves as a friction pump (97) for bringing a combustion gas exhaust gas temperature close to −273 ° C. However, in an all-blade gas turbine equipped with a water-repellent turbine blade, the outer compressor blade group (16) and the inner compressor blade group (17) each having an assembled structure by integrally casting (84) in an annular shape are large. An all- moving blade steam gas turbine integrated engine, characterized in that a water cooling vane (87) is provided in an annular shape in each section. 【請求項６７】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼蒸気ガスタービンにおいて、環状に一体
鋳造（８４）して組立構造とした夫々の外側圧縮機動翼
群（１６）及び内側圧縮機動翼群（１７）の大部分に、
水冷却翼（８７）を段落毎環状に設けたことを特徴とす
る全動翼蒸気ガスタービン合体機関。67. An outer shaft device and an inner shaft device that rotate in mutually opposite directions are combined at an optimum rotation ratio by a magnetic friction power transmission device (14) that also functions as a friction pump (97) for bringing the exhaust gas exhaust temperature close to −273 ° C. However, in an all-blade steam gas turbine equipped with a water-repellent turbine blade, each of the outer compressor blade group (16) and the inner compressor blade group (17) is integrally cast (84) in an annular shape to form an assembled structure. To a large extent,
A total moving blade steam gas turbine integrated engine, characterized in that a water cooling blade (87) is annularly provided for each paragraph. 【請求項６８】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼ガスタービンにおいて、環状に一体鋳
造（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けたことが特徴
の全動翼蒸気ガスタービン合体機関。68. A total moving blade gas comprising a water repellent turbine blade, in which an outer shaft device and an inner shaft device rotating in opposite directions are coupled at an optimum rotation ratio by a generator for making a combustion gas exhaust gas temperature close to −273 ° C. In the turbine, a water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally formed by annular casting (84). The all-blade steam gas turbine integrated engine characterized by being installed in each ring. 【請求項６９】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼蒸気ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造とした夫々の外側圧縮機動
翼群（１６）及び内側圧縮機動翼群（１７）の大部分に
撥水性水冷却翼（８７）を段落毎環状に設けたことが特
徴の全動翼蒸気ガスタービン合体機関。69. A full rotor blade steam comprising a water-repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions from each other, are combined at an optimum rotation ratio by a generator for making a combustion gas exhaust gas temperature close to −273 ° C. In a gas turbine, a water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally formed by annularly casting (84) into an assembled structure. The all-blade steam gas turbine integrated engine characterized by being installed in each ring. 【請求項７０】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼ガスタービン
において、環状に一体鋳造（８４）して組立構造とした
夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）の大部分に、撥水性水冷却翼（８７）を設け
て、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴
射手段（５６）より水噴射することを特徴とする全動翼
蒸気ガスタービン合体機関。70. A group of outer compressor blades each having an assembled structure integrally cast (84) in an annular shape in a full-blade gas turbine equipped with a water repellent turbine blade for making a combustion gas exhaust temperature close to −273 ° C. A water-repellent water cooling blade (87) is provided on most of the (16) and the inner compressor rotor blade group (17), and one or more water-repellent water cooling blades are cooled for each paragraph and then the water injection means (56) is used. A full-blade steam gas turbine integrated engine characterized by water injection. 【請求項７１】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼蒸気ガスター
ビンにおいて、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を設
けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水
噴射手段（５６）より水噴射することを特徴とする全動
翼蒸気ガスタービン合体機関。71. In an all-blade steam gas turbine equipped with a water-repellent turbine blade for bringing a combustion gas exhaust temperature close to -273 ° C., each outer compressor blade is integrally cast (84) in an annular shape to form an assembled structure. A water-repellent water cooling blade (87) is provided on most of the group (16) and the inner compressor rotor blade group (17), and water injection means (56) is provided after cooling one or more water-repellent water cooling blades per paragraph. A full-blade steam gas turbine combined engine characterized by more water injection. 【請求項７２】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼ガスタービンにおいて、環状に一体鋳造
（８４）して組立構造として、夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に撥水
性水冷却翼（８７）を設けて、段落毎１以上複数の撥水
性水冷却翼を冷却後に水噴射手段（５６）より水噴射す
ることを特徴とする全動翼蒸気ガスタービン合体機関。72. An outer shaft device and an inner shaft device that rotate in mutually opposite directions are coupled at an optimum rotation ratio by a magnetic friction power transmission device (14) that also functions as a friction pump (97) for bringing a combustion gas exhaust gas temperature close to -273 ° C. However, in a full-blade gas turbine equipped with a water-repellent turbine blade, the outer compressor blade group (16) and the inner compressor blade group (17) are respectively formed into a large size by integrally casting (84) in an annular shape to form an assembled structure. A water vapor repellent water cooling blade (87) is provided in a part, and water is injected from the water injection means (56) after cooling one or more water repellent water cooling blades per paragraph. organ. 【請求項７３】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼蒸気ガスタービンにおいて、環状に一体
鋳造（８４）して組立構造として、夫々の外側圧縮機動
翼群（１６）及び内側圧縮機動翼群（１７）の大部分
に、撥水性水冷却翼（８７）を設けて、段落毎１以上複
数の撥水性水冷却翼を冷却後に水噴射手段（５６）より
水噴射することを特徴とする全動翼蒸気ガスタービン合
体機関。73. An outer shaft device and an inner shaft device that rotate in opposite directions are coupled at an optimum rotation ratio by a magnetic friction power transmission device (14) that also functions as a friction pump (97) for bringing a combustion gas exhaust gas temperature close to −273 ° C. Then, in an all-blade steam gas turbine equipped with a water-repellent turbine blade, the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (16) and the inner compressor blade group (17) are integrally formed by annular casting (84). Mostly, a water-repellent water cooling blade (87) is provided, and one or more water-repellent water cooling blades for each paragraph are cooled and then water-injected by a water injection means (56). Turbine united engine. 【請求項７４】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼ガスタービンにおいて、環状に一体鋳
造（８４）して組立構造として、夫々の外側圧縮機動翼
群（１６）及び内側圧縮機動翼群（１７）の大部分に、
撥水性水冷却翼（８７）を設けて、段落毎１以上複数の
撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴
射することを特徴とする全動翼蒸気ガスタービン合体機
関。74. A full rotor blade gas comprising a water repellent turbine blade, in which an outer shaft device and an inner shaft device rotating in mutually opposite directions are coupled at an optimum rotation ratio by a generator for making a combustion gas exhaust temperature close to −273 ° C. In the turbine, as an assembled structure by integrally casting (84) in an annular shape, most of the outer compressor blade group (16) and the inner compressor blade group (17) are
A full-blade steam-gas turbine integrated engine, comprising a water-repellent water cooling blade (87), and water-injecting means (56) for injecting water after cooling one or more water-repellent water cooling blades for each paragraph. 【請求項７５】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼蒸気ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造として、夫々の外側圧縮機
動翼群（１６）及び内側圧縮機動翼群（１７）の大部分
に、撥水性水冷却翼（８７）を設けて、段落毎１以上複
数の撥水性水冷却翼を冷却後に水噴射手段（５６）より
水噴射することを特徴とする全動翼蒸気ガスタービン合
体機関。75. A full rotor blade steam comprising a water-repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions from each other, are connected at an optimum rotation ratio by a generator that brings a combustion gas exhaust gas temperature close to −273 ° C. In a gas turbine, a water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) as an assembled structure by integrally casting (84) in an annular shape. A full-blade steam gas turbine integrated engine, wherein one or more water-repellent water cooling blades are provided for each paragraph and water is injected from a water injection means (56) after cooling. 【請求項７６】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼ガスタービン
において、環状に一体鋳造（８４）して組立構造とし
て、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を設
けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に
水噴射手段（５６）より水噴射することを特徴とする全
動翼蒸気ガスタービン合体機関。76. A full-blade gas turbine equipped with water-repellent turbine blades, which brings a combustion gas exhaust temperature close to -273 ° C., is integrally cast (84) in an annular shape as an assembled structure to form a group of outer compressor blades. A water-repellent water cooling blade (87) is provided in most of the (16) and the inner compressor rotor blade group (17), and after cooling all or less than half of the water-repellent water cooling blade from the water injection means (56). A full-blade steam gas turbine integrated engine characterized by water injection. 【請求項７７】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼蒸気ガスター
ビンにおいて、環状に一体鋳造（８４）して組立構造と
して、夫々の外側圧縮機動翼群（１６）及び内側圧縮機
動翼群（１７）の大部分に、撥水性水冷却翼（８７）を
設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後
に水噴射手段（５６）より水噴射する撥水性水冷却翼
（８７）を含めたことを特徴とする全動翼蒸気ガスター
ビン合体機関。77. In an all moving blade steam gas turbine having a water repellent turbine blade for bringing a combustion gas exhaust temperature close to -273 [deg.] C., the outer compressor blades of each outer compressor are integrally cast (84) in an annular shape as an assembly structure. A water-repellent water cooling blade (87) is provided in most of the group (16) and the inner compressor rotor blade group (17), and water injection means (56) is provided after cooling all or less than half of the water-repellent water cooling blade in each paragraph. An all-blade steam gas turbine combined engine including a water-repellent water cooling blade (87) for more water injection. 【請求項７８】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼ガスタービンにおいて、環状に一体鋳造
（８４）して組立構造として、夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を設けて、段落毎全部以下半分の
撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴
射する撥水性水冷却翼（８７）を含めたことを特徴とす
る全動翼蒸気ガスタービン合体機関。78. An outer shaft device and an inner shaft device, which rotate in opposite directions, are combined at an optimum rotation ratio by a magnetic friction power transmission device (14) which also serves as a friction pump (97) for bringing a combustion gas exhaust gas temperature close to −273 ° C. However, in a full-blade gas turbine equipped with a water-repellent turbine blade, the outer compressor blade group (16) and the inner compressor blade group (17) are respectively formed into a large size by integrally casting (84) in an annular shape to form an assembled structure. A water-repellent water cooling blade (87) was provided in a part, and a water-repellent water cooling blade (87) for injecting water from the water injection means (56) after cooling all the water-repellent water cooling blades of not more than half each paragraph was included. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項７９】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼蒸気ガスタービンにおいて、環状に一体
鋳造（８４）して組立構造として、夫々の外側圧縮機動
翼群（１６）及び内側圧縮機動翼群（１７）の大部分
に、撥水性水冷却翼（８７）を設けて、段落毎全部以下
半分の撥水性水冷却翼を冷却後に水噴射手段（５６）よ
り水噴射する撥水性水冷却翼（８７）を含めたことを特
徴とする全動翼蒸気ガスタービン合体機関。79. An outer shaft device and an inner shaft device that rotate in mutually opposite directions are coupled at an optimum rotation ratio by a magnetic friction power transmission device (14) that also functions as a friction pump (97) for bringing a combustion gas exhaust gas temperature close to −273 ° C. Then, in an all-blade steam gas turbine equipped with a water-repellent turbine blade, the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (16) and the inner compressor blade group (17) are integrally formed by annular casting (84). Mostly, a water-repellent water cooling blade (87) is provided, and a water-repellent water cooling blade (87) for injecting water from the water injection means (56) after cooling the water-repellent water cooling blade of not more than half each paragraph is included. An all-blade steam gas turbine combined engine characterized by the above. 【請求項８０】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼ガスタービンにおいて、環状に一体鋳
造（８４）して組立構造として、夫々の外側圧縮機動翼
群（１６）及び内側圧縮機動翼群（１７）の大部分に、
撥水性水冷却翼（８７）を設けて、段落毎全部以下半分
の撥水性水冷却翼を冷却後に水噴射手段（５６）より水
噴射する撥水性水冷却翼（８７）を含めたことを特徴と
する全動翼蒸気ガスタービン合体機関。80. A rotor blade gas having a water-repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions from each other, are coupled at an optimum rotation ratio by a generator that brings a combustion gas exhaust gas temperature close to −273 ° C. In the turbine, as an assembled structure by integrally casting (84) in an annular shape, most of the outer compressor blade group (16) and the inner compressor blade group (17) are
A water-repellent water cooling blade (87) is provided, and a water-repellent water cooling blade (87) for injecting water from the water injection means (56) after cooling half or less water-repellent water cooling blades for each paragraph is included. Combined full-blade steam gas turbine engine. 【請求項８１】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼蒸気ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造として、夫々の外側圧縮機
動翼群（１６）及び内側圧縮機動翼群（１７）の大部分
に、撥水性水冷却翼（８７）を設けて、段落毎全部以下
半分の撥水性水冷却翼を冷却後に水噴射手段（５６）よ
り水噴射することを特徴とする全動翼蒸気ガスタービン
合体機関。81. A full rotor blade steam comprising a water-repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions from each other, are connected at an optimum rotation ratio by a generator that brings a combustion gas exhaust gas temperature close to -273 ° C. In a gas turbine, a water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) as an assembled structure by integrally casting (84) in an annular shape. A full moving blade steam gas turbine integrated engine, characterized in that water is injected from the water injection means (56) after cooling each of the water-repellent water cooling blades of not more than half in each paragraph. 【請求項８２】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼ガスタービン
において、環状に一体鋳造（８４）して組立構造とした
夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）の大部分に、撥水性水冷却翼（８７）を段落毎
環状に設けて、該出力で駆動する装置を具備したことを
特徴とする全動翼蒸気ガスタービン合体機関。82. In an all-blade gas turbine equipped with water-repellent turbine blades, the combustion gas exhaust temperature of which approaches −273 ° C., each outer compressor blade group having an assembled structure by integrally casting (84) in an annular shape. (16) and most of the inner compressor rotor blade group (17), a water-repellent water cooling blade (87) is provided in an annular shape for each paragraph, and a device driven by the output is provided. Steam gas turbine integrated engine. 【請求項８３】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼蒸気ガスター
ビンにおいて、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を段
落毎環状に設けて、該出力で駆動する装置を具備したこ
とを特徴とする全動翼蒸気ガスタービン合体機関。83. In an all-blade steam gas turbine equipped with a water-repellent turbine blade for bringing a combustion gas exhaust temperature close to -273.degree. C., each outer compressor blade is integrally cast (84) in an annular shape to form an assembled structure. Most of the group (16) and the inner compressor rotor blade group (17) are provided with a water repellent water cooling blade (87) in an annular shape for each paragraph, and equipped with a device driven by the output. Wing steam gas turbine combined engine. 【請求項８４】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼ガスタービンにおいて、環状に一体鋳造
（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けて、該出力で
駆動する装置を具備したことを特徴とする全動翼蒸気ガ
スタービン合体機関。84. An outer shaft device and an inner shaft device, which rotate in mutually opposite directions, are coupled at an optimum rotation ratio by a magnetic friction power transmission device (14) which also serves as a friction pump (97) for bringing a combustion gas exhaust gas temperature close to −273 ° C. However, in an all-blade gas turbine equipped with a water-repellent turbine blade, the outer compressor blade group (16) and the inner compressor blade group (17) each having an assembled structure by integrally casting (84) in an annular shape are large. A water-repellent water-cooling blade (87) is provided in each part in a ring shape in a portion thereof, and is equipped with a device driven by the output. 【請求項８５】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼蒸気ガスタービンにおいて、環状に一体
鋳造（８４）して組立構造とした夫々の外側圧縮機動翼
群（１６）及び内側圧縮機動翼群（１７）の大部分に、
撥水性水冷却翼（８７）を段落毎環状に設けて、該出力
で駆動する装置を具備したことを特徴とする全動翼蒸気
ガスタービン合体機関。85. An outer shaft device and an inner shaft device that rotate in mutually opposite directions are coupled at an optimum rotation ratio by a magnetic friction power transmission device (14) that also functions as a friction pump (97) for bringing a combustion gas exhaust gas temperature close to −273 ° C. However, in an all-blade steam gas turbine equipped with a water-repellent turbine blade, each of the outer compressor blade group (16) and the inner compressor blade group (17) is integrally cast (84) in an annular shape to form an assembled structure. To a large extent,
An all-blade steam gas turbine integrated engine, comprising a water-repellent water cooling blade (87) provided in an annular shape for each paragraph and equipped with a device driven by the output. 【請求項８６】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼ガスタービンにおいて、環状に一体鋳
造（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を段落毎環状に設けて、該出力で
駆動する装置を具備したことを特徴とする全動翼蒸気ガ
スタービン合体機関。86. A total moving blade gas comprising a water repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions from each other, are coupled at an optimum rotation ratio by a generator that brings a combustion gas exhaust gas temperature close to −273 ° C. In the turbine, a water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17), which are integrally formed by annular casting (84). An all-blade steam gas turbine integrated engine, characterized in that it is equipped with a device that is provided in each ring and is driven by the output. 【請求項８７】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼蒸気ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造とした夫々の外側圧縮機動
翼群（１６）及び内側圧縮機動翼群（１７）の大部分
に、撥水性水冷却翼（８７）を段落毎環状に設けて、該
出力で駆動する装置を具備したことを特徴とする全動翼
蒸気ガスタービン合体機関。87. A full rotor blade steam comprising a water-repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions from each other, are connected at an optimum rotation ratio by a generator that brings a combustion gas exhaust gas temperature close to −273 ° C. In the gas turbine, a water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) which are integrally formed by annularly casting (84) into an assembled structure. An all-blade steam gas turbine integrated engine, characterized in that each paragraph is provided in an annular shape and is equipped with a device driven by the output. 【請求項８８】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼ガスタービン
において、環状に一体鋳造（８４）して組立構造とした
夫々の外側圧縮機動翼群（１６）及び内側圧縮機動翼群
（１７）の大部分に、撥水性水冷却翼（８７）を設け
て、段落毎１以上複数の撥水性水冷却翼を冷却後に水噴
射手段（５６）より水噴射して、該出力で駆動する装置
を具備したことを特徴とする全動翼蒸気ガスタービン合
体機関。88. In an all-blade gas turbine equipped with water-repellent turbine blades, the combustion gas exhaust temperature of which approaches -273.degree. C., each outer compressor blade group having an assembled structure by integrally casting (84) in an annular shape. A water-repellent water cooling blade (87) is provided on most of the (16) and the inner compressor rotor blade group (17), and one or more water-repellent water cooling blades are cooled for each paragraph and then the water injection means (56) is used. An all-blade steam gas turbine integrated engine comprising a device for injecting water and driving with the output. 【請求項８９】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼蒸気ガスター
ビンにおいて、環状に一体鋳造（８４）して組立構造と
した夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を設
けて、段落毎１以上複数の撥水性水冷却翼を冷却後に水
噴射手段（５６）より水噴射して、該出力で駆動する装
置を具備したことを特徴とする全動翼蒸気ガスタービン
合体機関。89. In an all-blade steam gas turbine equipped with a water-repellent turbine blade for bringing a combustion gas exhaust temperature close to -273 ° C., each outer compressor blade is integrally cast (84) in an annular shape to form an assembled structure. A water-repellent water cooling blade (87) is provided on most of the group (16) and the inner compressor rotor blade group (17), and water injection means (56) is provided after cooling one or more water-repellent water cooling blades per paragraph. An all-blade steam-gas turbine integrated engine comprising a device for further water injection and driving with the output. 【請求項９０】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼ガスタービンにおいて、環状に一体鋳造
（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を設けて、段落毎１以上複数の撥
水性水冷却翼を冷却後に水噴射手段（５６）より水噴射
して、該出力で駆動する装置を具備したことを特徴とす
る全動翼蒸気ガスタービン合体機関。90. An outer shaft device and an inner shaft device that rotate in mutually opposite directions are coupled at an optimum rotation ratio by a magnetic friction power transmission device (14) that also functions as a friction pump (97) for bringing a combustion gas exhaust temperature close to −273 ° C. However, in an all-blade gas turbine equipped with a water-repellent turbine blade, the outer compressor blade group (16) and the inner compressor blade group (17) each having an assembled structure by integrally casting (84) in an annular shape are large. A water-repellent water cooling blade (87) was provided in the part, and after cooling one or more water-repellent water cooling blades in each paragraph, water jetting means (56) jetted water and equipped with a device for driving with this output. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項９１】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼蒸気ガスタービンにおいて、環状に一体
鋳造（８４）して組立構造とした夫々の外側圧縮動機翼
群（１６）及び内側圧縮機動翼群（１７）の大部分に、
撥水性水冷却翼（８７）を設けて、段落毎１以上複数の
撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴
射して、該出力で駆動する装置を具備したことを特徴と
する全動翼蒸気ガスタービン合体機関。91. An outer shaft device and an inner shaft device that rotate in mutually opposite directions are coupled at an optimum rotation ratio by a magnetic friction power transmission device (14) that also serves as a friction pump (97) for bringing a combustion gas exhaust temperature close to −273 ° C. However, in an all-blade steam gas turbine equipped with a water-repellent turbine blade, the outer compressor blade group (16) and the inner compressor blade group (17) of the outer compressor blade group (16) and the inner compressor blade group (17) which are integrally cast in an annular shape (84) and have an assembled structure To a large extent,
A water-repellent water cooling vane (87) is provided, and after each paragraph, one or more water-repellent water cooling vanes are cooled, and then water jetting means (56) jets water and drives with the output. Combined full-blade steam gas turbine engine. 【請求項９２】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼ガスタービンにおいて、環状に一体鋳
造（８４）して組立構造とした夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を設けて、段落毎１以上複数の撥
水性水冷却翼を冷却後に水噴射手段（５６）より水噴射
して、該出力で駆動する装置を具備したことを特徴とす
る全動翼蒸気ガスタービン合体機関。92. A total moving blade gas comprising a water repellent turbine blade, in which an outer shaft device and an inner shaft device rotating in mutually opposite directions are coupled at an optimum rotation ratio by a generator that brings a combustion gas exhaust gas temperature close to −273 ° C. In the turbine, a water-repellent water cooling blade (87) is provided on most of each of the outer compressor blade group (16) and the inner compressor blade group (17) which are integrally formed by annular casting (84). And a water-repellent water cooling vane for each paragraph is cooled, and a device for injecting water from a water injecting means (56) and driving with the output is provided. . 【請求項９３】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼蒸気ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造とした夫々の外側圧縮機動
翼群（１６）及び内側圧縮機動翼群（１７）の大部分
に、撥水性水冷却翼（８７）を設けて、段落毎１以上複
数の撥水性水冷却翼を冷却後に水噴射手段（５６）より
水噴射して、該出力で駆動する装置を具備したことを特
徴とする全動翼蒸気ガスタービン合体機関。93. A full rotor blade steam comprising a water-repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions from each other, are coupled at an optimum rotation ratio by a generator that brings a combustion gas exhaust gas temperature close to −273 ° C. In the gas turbine, a water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) which are integrally formed by annularly casting (84) into an assembled structure. A total moving blade steam gas turbine unit characterized in that it is provided with one or more water-repellent water cooling blades for each paragraph, after which water is injected from a water injection means (56) and driven by the output. organ. 【請求項９４】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼ガスタービン
において、環状に一体鋳造（８４）して組立構造とし
て、夫々の外側圧縮機動翼群（１６）及び内側圧縮機動
翼群（１７）の大部分に、撥水性水冷却翼（８７）を設
けて、段落毎全部以下半分の撥水性水冷却翼を冷却後に
水噴射手段（５６）より水噴射して、該出力で駆動する
装置を具備したことを特徴とする全動翼蒸気ガスタービ
ン合体機関。94. In a full-blade gas turbine having a water-repellent turbine blade, which brings a combustion gas exhaust gas temperature close to -273 ° C., is integrally cast (84) in an annular shape as an assembled structure to form a group of outer compressor blades. A water-repellent water cooling blade (87) is provided in most of the (16) and the inner compressor rotor blade group (17), and after cooling all or less than half of the water-repellent water cooling blade from the water injection means (56). An all-blade steam gas turbine integrated engine comprising a device for injecting water and driving with the output. 【請求項９５】 燃焼ガス排気温度を−２７３℃に近付
ける、撥水性タービン翼を具備した全動翼蒸気ガスター
ビンにおいて、環状に一体鋳造（８４）して組立構造と
して、夫々の外側圧縮機動翼群（１６）及び内側圧縮機
動翼群（１７）の大部分に、撥水性水冷却翼（８７）を
設けて、段落毎全部以下半分の撥水性水冷却翼を冷却後
に水噴射手段（５６）より水噴射して、該出力で駆動す
る装置を具備したことを特徴とする全動翼蒸気ガスター
ビン合体機関。95. In an all-blade steam gas turbine equipped with a water-repellent turbine blade for bringing a combustion gas exhaust temperature close to −273 ° C., the outer compressor blades of each outer compressor are integrally cast (84) in an annular shape as an assembly structure. A water-repellent water cooling blade (87) is provided in most of the group (16) and the inner compressor rotor blade group (17), and water injection means (56) is provided after cooling all or less than half of the water-repellent water cooling blade in each paragraph. An all-blade steam-gas turbine integrated engine comprising a device for further water injection and driving with the output. 【請求項９６】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼ガスタービンにおいて、環状に一体鋳造
（８４）して組立構造として、夫々の外側圧縮機動翼群
（１６）及び内側圧縮機動翼群（１７）の大部分に、撥
水性水冷却翼（８７）を設けて、段落毎全部以下半分の
撥水性水冷却翼を冷却後に水噴射手段（５６）より水噴
射して、該出力で駆動する装置を具備したことを特徴と
する全動翼蒸気ガスタービン合体機関。96. An outer shaft device and an inner shaft device which rotate in opposite directions are coupled at an optimum rotation ratio by a magnetic friction power transmission device (14) which also serves as a friction pump (97) for bringing a combustion gas exhaust gas temperature close to −273 ° C. However, in a full-blade gas turbine equipped with a water-repellent turbine blade, the outer compressor blade group (16) and the inner compressor blade group (17) are respectively formed into a large size by integrally casting (84) in an annular shape to form an assembled structure. A water-repellent water cooling vane (87) was provided in a part, and after each paragraph, less than half of the water-repellent water cooling vanes were cooled, and water was jetted from the water jetting means (56) to be driven by the output. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項９７】 燃焼ガス排気温度を−２７３℃に近付
ける摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装置
（１４）により互いに反対方向に回転する外側軸装置と
内側軸装置を最適回転比で結合し、撥水性タービン翼を
具備した全動翼蒸気ガスタービンにおいて、環状に一体
鋳造（８４）して組立構造として、夫々の外側圧縮動機
翼群（１６）及び内側圧縮機動翼群（１７）の大部分
に、撥水性水冷却翼（８７）を設けて、段落毎全部以下
半分の撥水性水冷却翼を冷却後に水噴射手段（５６）よ
り水噴射して、該出力で駆動する装置を具備したことを
特徴とする全動翼蒸気ガスタービン合体機関。97. An outer shaft device and an inner shaft device, which rotate in mutually opposite directions, are connected at an optimum rotation ratio by a magnetic friction power transmission device (14) which also functions as a friction pump (97) for bringing a combustion gas exhaust gas temperature close to −273 ° C. Then, in an all-blade steam gas turbine equipped with a water-repellent turbine blade, the outer compression motor blade group (16) and the inner compressor blade group (17) of the outer compression motor blade group (16) and the inner compressor blade group (17) are integrally formed by annular casting (84). Mostly, a water-repellent water cooling blade (87) is provided, and after each paragraph, less than half of the water-repellent water cooling blades are cooled and then water-injecting means (56) injects water to drive with the output. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項９８】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼ガスタービンにおいて、環状に一体鋳
造（８４）して組立構造として、夫々の外側圧縮機動翼
群（１６）及び内側圧縮機動翼群（１７）の大部分に、
撥水性水冷却翼（８７）を設けて、段落毎全部以下半分
の撥水性水冷却翼を冷却後に水噴射手段（５６）より水
噴射して、該出力で駆動する装置を具備したことを特徴
とする全動翼蒸気ガスタービン合体機関。98. A total moving blade gas comprising a water repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions from each other, are connected at an optimum rotation ratio by a generator that brings a combustion gas exhaust gas temperature close to −273 ° C. In the turbine, as an assembled structure by integrally casting (84) in an annular shape, most of the outer compressor blade group (16) and the inner compressor blade group (17) are
A water-repellent water cooling blade (87) is provided, and after each paragraph half or less of the water-repellent water cooling blade is cooled, water is injected from the water injection means (56), and a device for driving with the output is provided. Combined full-blade steam gas turbine engine. 【請求項９９】 燃焼ガス排気温度を−２７３℃に近付
ける発電機により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼蒸気ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造として、夫々の外側圧縮機
動翼群（１６）及び内側圧縮機動翼群（１７）の大部分
に、撥水性水冷却翼（８７）を設けて、段落毎全部以下
半分の水冷却翼を冷却後に水噴射手段（５６）より水噴
射して、該出力で駆動する装置を具備したことを特徴と
する全動翼蒸気ガスタービン合体機関。99. A full rotor blade steam comprising a water repellent turbine blade, in which an outer shaft device and an inner shaft device that rotate in mutually opposite directions are coupled at an optimum rotation ratio by a generator that makes a combustion gas exhaust gas temperature close to -273 ° C. In a gas turbine, a water-repellent water cooling blade (87) is provided on most of the outer compressor blade group (16) and the inner compressor blade group (17) as an assembled structure by integrally casting (84) in an annular shape. An all-blade steam-gas turbine integrated engine, characterized in that it is provided with a device that is provided and injects water by the water injection means (56) after cooling all or less than half of the water-cooling blades for each paragraph, and drives with this output. 【請求項１００】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンにおい
て、環状に一体鋳造（８４）して組立構造とした内側タ
ービン動翼群（２０）に、水噴射手段（５６ａ）を設け
たことを特徴とする全動翼蒸気ガスタービン合体機関。100. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. In a full-blade steam gas turbine, a water-injection means (56a) is provided in an inner turbine bucket group (20) that is integrally cast (84) in an annular shape and has an assembled structure. Turbine united engine. 【請求項１０１】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンにおい
て、環状に一体鋳造（８４）して組立構造とした外側タ
ービン動翼群（１９）に、水噴射手段（５６ａ）を設け
たことを特徴とする全動翼蒸気ガスタービン合体機関。101. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. In a full-blade steam gas turbine, a water-injection means (56a) is provided in an outer turbine bucket group (19) that is integrally cast (84) in an annular shape and has an assembled structure, Turbine united engine. 【請求項１０２】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンにおいて、
環状に一体鋳造（８４）して組立構造とした内側タービ
ン動翼群（２０）に、水噴射手段（５６ａ）を設けたこ
とを特徴とする全動翼蒸気ガスタービン合体機関。102. A water repellent turbine blade is provided, wherein an outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio. In a full-blade gas turbine,
A total moving blade steam gas turbine integrated engine, wherein a water injection means (56a) is provided on an inner turbine rotor blade group (20) which is integrally cast (84) in an annular shape and has an assembled structure. 【請求項１０３】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンにおいて、
環状に一体鋳造（８４）して組立構造とした外側タービ
ン動翼群（１９）に、水噴射手段（５６ａ）を設けたこ
とを特徴とする全動翼蒸気ガスタービン合体機関。103. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. In a full-blade gas turbine,
An all-blade steam-gas turbine integrated engine, characterized in that a water injection means (56a) is provided in an outer turbine rotor blade group (19) that is integrally cast (84) in an annular shape and has an assembled structure. 【請求項１０４】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンにおいて、
環状に一体鋳造（８４）して組立構造とした内側タービ
ン動翼群（２０）に、水噴射手段（５６ａ）を設けたこ
とを特徴とする全動翼蒸気ガスタービン合体機関。104. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. In a full-blade steam turbine,
A total moving blade steam gas turbine integrated engine, wherein a water injection means (56a) is provided on an inner turbine rotor blade group (20) which is integrally cast (84) in an annular shape and has an assembled structure. 【請求項１０５】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンにおいて、
環状に一体鋳造（８４）して組立構造とした外側タービ
ン動翼群（１９）に、水噴射手段（５６ａ）を設けたこ
とを特徴とする全動翼蒸気ガスタービン合体機関。105. A magnetic repulsive power transmission device (14), which also serves as a friction pump (97), connects an outer shaft device and an inner shaft device that rotate in opposite directions to each other at an optimum rotation ratio, and comprises a water repellent turbine blade. In a full-blade steam turbine,
An all-blade steam-gas turbine integrated engine, characterized in that a water injection means (56a) is provided in an outer turbine rotor blade group (19) that is integrally cast (84) in an annular shape and has an assembled structure. 【請求項１０６】 発電機により互いに反対方向に回転
する外側軸装置と内側軸装置を最適回転比で結合し、撥
水性タービン翼を具備した全動翼蒸気ガスタービンにお
いて、環状に一体鋳造（８４）して組立構造とした内側
タービン動翼群（２０）の組立環状接続部付近に、水噴
射手段（５６ａ）を断熱して設けたことを特徴とする全
動翼蒸気ガスタービン合体機関。106. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, and are integrally cast in an annular shape (84). ), The water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) in a thermally insulated manner, and the all-blade steam gas turbine integrated engine is provided. 【請求項１０７】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンにおいて、環状に一体鋳造（８４）し
て組立構造とした内側タービン動翼群（２０）の組立環
状接続部付近に、水噴射手段（５６ａ）を断熱して設け
たことを特徴とする全動翼蒸気ガスタービン合体機関。107. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, a water is provided near an assembled annular connecting portion of an inner turbine blade group (20) which is integrally formed by annular casting (84) to form an assembled structure. An all-blade steam gas turbine combined engine, characterized in that the injection means (56a) is provided with heat insulation. 【請求項１０８】 発電機により互いに反対方向に回転
する外側軸装置と内側軸装置を最適回転比で結合し、撥
水性タービン翼を具備した全動翼蒸気ガスタービンにお
いて、環状に一体鋳造（８４）して組立構造とした外側
タービン動翼群（１９）の組立環状接続部付近に、水噴
射手段（５６ａ）を断熱して設けたことを特徴とする全
動翼蒸気ガスタービン合体機関。108. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, and are integrally cast in an annular shape (84). The water jet means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) having the above-described assembled structure with heat insulation provided. 【請求項１０９】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンにおいて、環状に一体鋳造（８４）し
て組立構造とした外側タービン動翼群（１９）の組立環
状接続部付近に、水噴射手段（５６ａ）を断熱して設け
たことを特徴とする全動翼蒸気ガスタービン合体機関。109. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, water is provided near an assembled annular connection portion of an outer turbine rotor blade group (19) which is integrally formed by annular casting (84) into an assembled structure. An all-blade steam gas turbine combined engine, characterized in that the injection means (56a) is provided with heat insulation. 【請求項１１０】 発電機により互いに反対方向に回転
する外側軸装置と内側軸装置を最適回転比で結合し、撥
水性タービン翼を具備した全動翼ガスタービンにおい
て、環状に一体鋳造（８４）して組立構造とした内側タ
ービン動翼群（２０）の組立環状接続部付近に、水噴射
手段（５６ａ）を断熱して設けたことを特徴とする全動
翼蒸気ガスタービン合体機関。110. In an all-blade gas turbine equipped with a water-repellent turbine blade, an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, and integrally cast in an annular shape (84). A water-jet injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) having the above-described assembled structure with heat insulation provided, and the all-blade steam gas turbine integrated engine is provided. 【請求項１１１】 撥水性タービン翼を具備した全動翼
ガスタービンにおいて、環状に一体鋳造（８４）して組
立構造とした内側タービン動翼群（２０）の組立環状接
続部付近に、水噴射手段（５６ａ）を断熱して設けたこ
とを特徴とする全動翼蒸気ガスタービン合体機関。111. In an all-blade gas turbine equipped with a water-repellent turbine blade, a water jet is provided in the vicinity of an assembled annular connecting portion of an inner turbine blade group (20) which is integrally cast in an annular shape (84) to form an assembled structure. An all-blade steam gas turbine integrated engine, characterized in that the means (56a) is provided with heat insulation. 【請求項１１２】 発電機により互いに反対方向に回転
する外側軸装置と内側軸装置を最適回転比で結合し、撥
水性タービン翼を具備した全動翼ガスタービンにおい
て、環状に一体鋳造（８４）して組立構造とした外側タ
ービン動翼群（１９）の組立環状接続部付近に、水噴射
手段（５６ａ）を断熱して設けたことを特徴とする全動
翼蒸気ガスタービン合体機関。112. In an all-blade gas turbine equipped with a water repellent turbine blade, an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, and are integrally cast in an annular shape (84). A water-jet injection means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) having an assembled structure by heat-insulating the water-injection means (56a). 【請求項１１３】 撥水性タービン翼を具備した全動翼
ガスタービンにおいて、環状に一体鋳造（８４）して組
立構造とした外側タービン動翼群（１９）の組立環状接
続部付近に、水噴射手段（５６ａ）を断熱して設けたこ
とを特徴とする全動翼蒸気ガスタービン合体機関。113. In a full-blade gas turbine equipped with a water-repellent turbine blade, a water jet is provided in the vicinity of an assembled annular connection portion of an outer turbine blade group (19) which is integrally cast (84) in an annular shape to form an assembled structure. An all-blade steam gas turbine integrated engine, characterized in that the means (56a) is provided with heat insulation. 【請求項１１４】 発電機により互いに反対方向に回転
する外側軸装置と内側軸装置を最適回転比で結合し、撥
水性タービン翼を具備した全動翼蒸気タービンにおい
て、環状に一体鋳造（８４）して組立構造とした内側タ
ービン動翼群（２０）の組立環状接続部付近に、水噴射
手段（５６ａ）を断熱して設けたことを特徴とする全動
翼蒸気ガスタービン合体機関。114. In an all-blade steam turbine equipped with a water repellent turbine blade, an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, and are integrally cast in an annular shape (84). A water-jet injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) having the above-described assembled structure with heat insulation provided, and the all-blade steam gas turbine integrated engine is provided. 【請求項１１５】 撥水性タービン翼を具備した全動翼
蒸気タービンにおいて、環状に一体鋳造（８４）して組
立構造とした内側タービン動翼群（２０）の組立環状接
続部付近に、水噴射手段（５６ａ）を断熱して設けたこ
とを特徴とする全動翼蒸気ガスタービン合体機関。115. In an all-blade steam turbine equipped with a water-repellent turbine blade, a water jet is provided near an assembled annular connecting portion of an inner turbine blade group (20) which is integrally cast (84) in an annular shape and has an assembled structure. An all-blade steam gas turbine integrated engine, characterized in that the means (56a) is provided with heat insulation. 【請求項１１６】 発電機により互いに反対方向に回転
する外側軸装置と内側軸装置を最適回転比で結合し、撥
水性タービン翼を具備した全動翼蒸気タービンにおい
て、環状に一体鋳造（８４）して組立構造とした外側タ
ービン動翼群（１９）の組立環状接続部付近に、水噴射
手段（５６ａ）を断熱して設けたことを特徴とする全動
翼蒸気ガスタービン合体機関。116. In an all-blade steam turbine equipped with a water-repellent turbine blade, an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, and are integrally cast in an annular shape (84). A water-jet injection means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) having an assembled structure by heat-insulating the water-injection means (56a). 【請求項１１７】 摩擦ポンプ（９７）兼用の磁気摩擦
動力伝達装置（１４）により互いに反対方向に回転する
外側軸装置と内側軸装置を最適回転比で結合し、撥水性
タービン翼を具備した全動翼蒸気ガスタービンにおい
て、環状に一体鋳造（８４）して組立構造とした内側タ
ービン動翼群（２０）の組立環状接続部付近に、水噴射
手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該
容積を縮小し単位質量を増大することを特徴とする全動
翼蒸気ガスタービン合体機関。117. A magnetic friction power transmission device (14) which also serves as a friction pump (97) is used to couple an outer shaft device and an inner shaft device that rotate in opposite directions to each other at an optimum rotation ratio, and a water repellent turbine blade is provided. In a moving blade steam gas turbine, superheated steam is provided by heat-insulating water injection means (56a) in the vicinity of an assembled annular connecting portion of an inner turbine moving blade group (20) integrally formed by casting (84) in an annular shape. Is cooled, the volume is reduced, and the unit mass is increased. 【請求項１１８】 摩擦ポンプ（９７）兼用の磁気摩擦
動力伝達装置（１４）により互いに反対方向に回転する
外側軸装置と内側軸装置を最適回転比で結合し、撥水性
タービン翼を具備した全動翼ガスタービンにおいて、環
状に一体鋳造（８４）して組立構造とした内側タービン
動翼群（２０）の組立環状接続部付近に、水噴射手段
（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積
を縮小し単位質量を増大することを特徴とする全動翼蒸
気ガスタービン合体機関。118. A magnetic friction power transmission device (14) which also functions as a friction pump (97) connects an outer shaft device and an inner shaft device, which rotate in mutually opposite directions, at an optimum rotation ratio, and is equipped with a water repellent turbine blade. In a rotor blade gas turbine, water injection means (56a) is provided in the vicinity of an assembled annular connection portion of an inner turbine rotor blade group (20) that is integrally cast (84) in an annular shape to construct a superheated steam. A full-blade steam gas turbine integrated engine, which is cooled to reduce its volume and increase its unit mass. 【請求項１１９】 摩擦ポンプ（９７）兼用の磁気摩擦
動力伝達装置（１４）により互いに反対方向に回転する
外側軸装置と内側軸装置を最適回転比で結合し、撥水性
タービン翼を具備した全動翼蒸気タービンにおいて、環
状に一体鋳造（８４）して組立構造とした内側タービン
動翼群（２０）の組立環状接続部付近に、水噴射手段
（５６ａ）を断熱して設けて過熱蒸気を冷却し、該容積
を縮小し単位質量を増大することを特徴とする全動翼蒸
気ガスタービン合体機関。119. A magnetic friction power transmission device (14) which also functions as a friction pump (97) connects an outer shaft device and an inner shaft device that rotate in opposite directions to each other at an optimum rotation ratio, and comprises a water repellent turbine blade. In the moving blade steam turbine, water injection means (56a) is provided near the assembled annular connection portion of the inner turbine moving blade group (20) that is integrally cast (84) in an annular shape to construct the superheated steam. A full-blade steam gas turbine integrated engine, which is cooled to reduce its volume and increase its unit mass. 【請求項１２０】 発電機により互いに反対方向に回転
する外側軸装置と内側軸装置を最適回転比で結合し、撥
水性タービン翼を具備した全動翼蒸気ガスタービンにお
いて、環状に一体鋳造（８４）して組立構造とした内側
タービン動翼群（２０）の組立環状接続部付近に、水噴
射手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、
該容積を縮小し単位質量を増大することを特徴とする全
動翼蒸気ガスタービン合体機関。120. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, and are integrally cast in an annular shape (84). ), The water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) in a thermally insulated manner to cool the superheated steam,
A full-blade steam gas turbine integrated engine characterized by reducing the volume and increasing the unit mass. 【請求項１２１】 発電機により互いに反対方向に回転
する外側軸装置と内側軸装置を最適回転比で結合し、撥
水性タービン翼を具備した全動翼ガスタービンにおい
て、環状に一体鋳造（８４）して組立構造とした内側タ
ービン動翼群（２０）の組立環状接続部付近に、水噴射
手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該
容積を縮小し単位質量を増大することを特徴とする全動
翼蒸気ガスタービン合体機関。121. In an all-blade gas turbine equipped with a water-repellent turbine blade, an outer shaft device and an inner shaft device, which are rotated in opposite directions by a generator, are coupled at an optimum rotation ratio, and integrally cast in an annular shape (84). The water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) having an assembled structure by heat insulation to cool the superheated steam, thereby reducing the volume and increasing the unit mass. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項１２２】 発電機により互いに反対方向に回転
する外側軸装置と内側軸装置を最適回転比で結合し、撥
水性タービン翼を具備した全動翼蒸気タービンにおい
て、環状に一体鋳造（８４）して組立構造とした内側タ
ービン動翼群（２０）の組立環状接続部付近に、水噴射
手段（５６ａ）を断熱して設けて過熱蒸気を冷却し、該
容積を縮小し単位質量を増大することを特徴とする全動
翼蒸気ガスタービン合体機関。122. In an all-blade steam turbine equipped with a water-repellent turbine blade, an outer shaft device and an inner shaft device, which rotate in opposite directions from each other by a generator, are coupled at an optimum rotation ratio, and are integrally cast in an annular shape (84). The water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) having an assembled structure by heat insulation to cool the superheated steam, thereby reducing the volume and increasing the unit mass. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項１２３】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装
置（１４）により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼蒸気ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造とした内側タービン動翼群
（２０）の組立環状接続部付近に、水噴射手段（５６
ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小
し単位質量を増大することを特徴とする全動翼蒸気ガス
タービン合体機関。123. An outer shaft device and an inner shaft device, which rotate in opposite directions by a magnetic friction power transmission device (14) which also functions as a friction pump (97), which brings a combustion gas exhaust gas temperature close to −273 ° C., have an optimum rotation ratio. In an all-blade steam gas turbine having a water-repellent turbine blade combined with each other, water injection means is provided in the vicinity of an assembled annular connecting portion of an inner turbine rotor blade group (20) which is integrally cast (84) in an annular shape and has an assembled structure. (56
An all-blade steam gas turbine integrated engine, characterized in that a) is provided so as to be heat-insulated to cool superheated steam to reduce the volume and increase the unit mass. 【請求項１２４】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装
置（１４）により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼蒸気ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造とした外側タービン動翼群
（１９）の組立環状接続部付近に、水噴射手段（５６
ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮小
し単位質量を増大することを特徴とする全動翼蒸気ガス
タービン合体機関。124. An outer shaft device and an inner shaft device, which rotate in mutually opposite directions by a magnetic friction power transmission device (14) which also serves as a friction pump (97) and which makes the combustion gas exhaust gas temperature approach -273 ° C., have an optimum rotation ratio. In an all-blade steam gas turbine having a water-repellent turbine blade combined with each other, water injection means is provided in the vicinity of an assembled annular connection portion of an outer turbine blade group (19) that is integrally cast (84) into an assembled structure. (56
An all-blade steam gas turbine integrated engine, characterized in that a) is provided so as to be heat-insulated to cool superheated steam to reduce the volume and increase the unit mass. 【請求項１２５】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装
置（１４）により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼ガスタービンにおいて、環状に一体鋳
造（８４）して組立構造とした内側タービン動翼群（２
０）の組立環状接続部付近に、水噴射手段（５６ａ）を
断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位
質量を増大することを特徴とする全動翼蒸気ガスタービ
ン合体機関。125. An outer shaft device and an inner shaft device, which rotate in mutually opposite directions by a magnetic friction power transmission device (14) which also functions as a friction pump (97), which brings a combustion gas exhaust gas temperature close to −273 ° C., have an optimum rotation ratio. In an all-blade gas turbine combined with water-repellent turbine blades, an inner turbine rotor blade group (2
0) Water-injection means (56a) is provided near the assembled annular connection part to cool the combustion gas to reduce the volume thereof and increase the unit mass. organ. 【請求項１２６】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の磁気摩擦動力伝達装
置（１４）により互いに反対方向に回転する外側軸装置
と内側軸装置を最適回転比で結合し、撥水性タービン翼
を具備した全動翼ガスタービンにおいて、環状に一体鋳
造（８４）して組立構造とした外側タービン動翼群（１
９）の組立環状接続部付近に、水噴射手段（５６ａ）を
断熱して設けて燃焼ガスを冷却し、該容積を縮小し単位
質量を増大することを特徴とする全動翼蒸気ガスタービ
ン合体機関。126. An outer shaft device and an inner shaft device, which rotate in opposite directions by a magnetic friction power transmission device (14) which also functions as a friction pump (97), which makes a combustion gas exhaust gas temperature close to −273 ° C., have an optimum rotation ratio. In an all-blade gas turbine combined with a water-repellent turbine blade, an outer turbine blade group (1
9) A water-jet injection means (56a) is provided near the assembled annular connection portion so as to be heat-insulated to cool the combustion gas, thereby reducing the volume and increasing the unit mass. organ. 【請求項１２７】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼蒸気ガスタービンにおいて、環状
に一体鋳造（８４）して組立構造とした内側タービン動
翼群（２０）の組立環状接続部付近に、水噴射手段（５
６ａ）を断熱して設けて過熱蒸気を冷却し、該容積を縮
小し単位質量を増大することを特徴とする全動翼蒸気ガ
スタービン合体機関。127. A rotor blade having a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are coupled at an optimum rotation ratio, and a combustion gas exhaust temperature approaches −273 ° C. In the steam gas turbine, the water injection means (5) is provided near the assembled annular connection portion of the inner turbine blade group (20) which is integrally cast (84) in an annular shape to form an assembled structure.
6a) is provided so as to be heat-insulated to cool the superheated steam to reduce the volume thereof and increase the unit mass thereof. 【請求項１２８】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼蒸気ガスタービンにおいて、環状
に一体鋳造（８４）して組立構造とした外側タービン動
翼群（１９）の組立環状接続部付近に、水噴射手段（５
６ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、
該容積を縮小し単位質量を増大することを特徴とする全
動翼蒸気ガスタービン合体機関。128. A total rotor blade having a water repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are combined at an optimum rotation ratio, and a combustion gas exhaust temperature approaches −273 ° C. In the steam gas turbine, water injection means (5) is provided near the assembled annular connection portion of the outer turbine rotor blade group (19) that is integrally cast (84) in an annular shape to form an assembled structure.
6a) is provided with heat insulation to cool superheated steam and combustion gas,
A full-blade steam gas turbine integrated engine characterized by reducing the volume and increasing the unit mass. 【請求項１２９】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造とした内側タービン動翼群
（２０）の組立環状接続部付近に、水噴射手段（５６
ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小
し単位質量を増大することを特徴とする全動翼蒸気ガス
タービン合体機関。129. A total rotor blade having a water repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are combined at an optimum rotation ratio, the combustion gas exhaust gas temperature approaching −273 ° C. In the gas turbine, water injection means (56) is provided near the assembled annular connection portion of the inner turbine rotor blade group (20) that is integrally cast (84) in an annular shape to form an assembled structure.
An all-blade steam gas turbine integrated engine characterized in that (a) is provided so as to be heat-insulated to cool the combustion gas to reduce the volume and increase the unit mass. 【請求項１３０】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造とした外側タービン動翼群
（１９）の組立環状接続部付近に、水噴射手段（５６
ａ）を断熱して設けて燃焼ガスを冷却し、該容積を縮小
し単位質量を増大することを特徴とする全動翼蒸気ガス
タービン合体機関。130. A total rotor blade having a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are combined at an optimum rotation ratio, and a combustion gas exhaust temperature approaches −273 ° C. In the gas turbine, the water injection means (56) is provided near the assembled annular connecting portion of the outer turbine blade group (19) that is integrally cast (84) in an annular shape to form an assembled structure.
An all-blade steam gas turbine integrated engine characterized in that (a) is provided so as to be heat-insulated to cool the combustion gas to reduce the volume and increase the unit mass. 【請求項１３１】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼蒸気ガスタ
ービンにおいて、環状に一体鋳造（８４）して組立構造
とした内側タービン動翼群（２０）の組立環状接続部付
近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気
や燃焼ガスを冷却し、該容積を縮小し単位質量を増大す
ることを特徴とする全動翼蒸気ガスタービン合体機関。131. In an all-blade steam gas turbine equipped with a water-repellent turbine blade for making a combustion gas exhaust gas temperature close to -273 ° C., an inner turbine blade group ( 20) Water-injecting means (56a) is provided near the assembled annular connection part so as to insulate it to cool superheated steam and combustion gas, thereby reducing the volume and increasing the unit mass. Gas turbine united engine. 【請求項１３２】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼蒸気ガスタ
ービンにおいて、環状に一体鋳造（８４）して組立構造
とした外側タービン動翼群（１９）の組立環状接続部付
近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気
や燃焼ガスを冷却し、該容積を縮小し単位質量を増大す
ることを特徴とする全動翼蒸気ガスタービン合体機関。132. In a full-blade steam gas turbine having a water-repellent turbine blade for making a combustion gas exhaust temperature close to −273 ° C., an outer turbine blade group () integrally assembled (84) in an annular shape to form an assembled structure ( 19) Water-injection means (56a) is provided near the assembled annular connection part to insulate it to cool superheated steam and combustion gas, and reduce the volume to increase the unit mass. Gas turbine united engine. 【請求項１３３】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼ガスタービ
ンにおいて、環状に一体鋳造（８４）して組立構造とし
た内側タービン動翼群（２０）の組立環状接続部付近
に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを
冷却し、該容積を縮小し単位質量を増大することを特徴
とする全動翼蒸気ガスタービン合体機関。133. An inner turbine blade group (20) having an assembled structure by integrally casting (84) in an annular shape in a full-blade gas turbine provided with a water-repellent turbine blade for making a combustion gas exhaust temperature close to −273 ° C. ), The water injection means (56a) is provided near the assembled annular connection so as to cool the combustion gas to reduce the volume and increase the unit mass. . 【請求項１３４】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼ガスタービ
ンにおいて、環状に一体鋳造（８４）して組立構造とし
た外側タービン動翼群（１９）の組立環状接続部付近
に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを
冷却し、該容積を縮小し単位質量を増大することを特徴
とする全動翼蒸気ガスタービン合体機関。134. A group of outer turbine blades (19) which are integrally cast (84) in an annular shape in an all-blade gas turbine equipped with a water-repellent turbine blade for making a combustion gas exhaust temperature close to -273 ° C. ), The water injection means (56a) is provided near the assembled annular connection so as to cool the combustion gas to reduce the volume and increase the unit mass. . 【請求項１３５】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼ガスタービ
ンにおいて、環状に一体鋳造（８４）して組立構造とし
た内側タービン動翼群（２０）の組立環状接続部付近
に、水噴射手段（５６ａ）を断熱して設けて燃焼ガスを
冷却し、該出力で駆動する装置を具備したことを特徴と
する全動翼蒸気ガスタービン合体機関。135. A full-blade gas turbine equipped with water-repellent turbine blades, which brings a combustion gas exhaust gas temperature close to −273 ° C., has an inner turbine blade group (20) integrally cast (84) into an assembled structure. ), A water-injection means (56a) is provided near the assembled annular connection portion to cool the combustion gas, and a device for driving with this output is provided. 【請求項１３６】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼ガスタービ
ンにおいて、環状に一体鋳造（８４）して組立構造とし
た外側タービン動翼群（１９）の組立環状接続部付近
に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気や
燃焼ガスを冷却し、該出力で駆動する装置を具備したこ
とを特徴とする全動翼蒸気ガスタービン合体機関。136. A group of outer turbine blades (19) having an assembled structure by integrally casting (84) in an annular shape in a full-blade gas turbine having a water-repellent turbine blade that brings a combustion gas exhaust temperature close to -273 ° C. ), A water-injection means (56a) is provided near the assembled annular connection to cool the superheated steam and combustion gas, and a device for driving with this output is provided. Coalescing agency. 【請求項１３７】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼蒸気ガスタ
ービンにおいて、環状に一体鋳造（８４）して組立構造
とした内側タービン動翼群（２０）の組立環状接続部付
近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気
や燃焼ガスを冷却し、該出力で駆動する装置を具備した
ことを特徴とする全動翼蒸気ガスタービン合体機関。137. In an all-blade steam gas turbine equipped with a water-repellent turbine blade for making a combustion gas exhaust temperature close to -273 ° C., an inner turbine blade group ( 20) A water jet means (56a) is provided in the vicinity of the assembled annular connection part so as to be heat-insulated to cool superheated steam and combustion gas, and a device for driving with this output is provided. Turbine united engine. 【請求項１３８】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼蒸気ガスタ
ービンにおいて、環状に一体鋳造（８４）して組立構造
とした外側タービン動翼群（１９）の組立環状接続部付
近に、水噴射手段（５６ａ）を断熱して設けて過熱蒸気
や燃焼ガスを冷却し、該出力で駆動する装置を具備した
ことを特徴とする全動翼蒸気ガスタービン合体機関。138. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, which makes a combustion gas exhaust temperature close to -273 ° C., an outer turbine blade group ( 19) A water jet means (56a) is provided near the assembled annular connection part so as to be heat-insulated to cool superheated steam and combustion gas, and a device for driving with this output is provided. Turbine united engine. 【請求項１３９】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の、磁気摩擦動力伝達
装置（１４）により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼ガスタービンにおいて、環状に一体
鋳造（８４）して組立構造とした内側タービン動翼群
（２０）の組立環状接続部付近に、水噴射手段（５６
ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動
する装置を具備したことを特徴とする全動翼蒸気ガスタ
ービン合体機関。139. An optimum rotation ratio of an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also serves as a friction pump (97) and that makes a combustion gas exhaust temperature close to −273 ° C. In a full-blade gas turbine having a water-repellent turbine blade, the water injection means is provided in the vicinity of an assembled annular connection portion of an inner turbine blade group (20) integrally cast (84) into an assembled structure. (56
An all-blade steam gas turbine integrated engine, which is equipped with a device for a) being adiabatically provided to cool the combustion gas and to be driven by the output. 【請求項１４０】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の、磁気摩擦動力伝達
装置（１４）により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼ガスタービンにおいて、環状に一体
鋳造（８４）して組立構造とした外側タービン動翼群
（１９）の組立環状接続部付近に、水噴射手段（５６
ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動
する装置を具備したことを特徴とする全動翼蒸気ガスタ
ービン合体機関。140. An optimum rotation ratio of an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also serves as a friction pump (97) and that makes the combustion gas exhaust temperature close to -273 ° C. In a full-blade gas turbine having a water-repellent turbine blade, the water-injection means is provided in the vicinity of the assembled annular connecting portion of the outer turbine blade group (19) that is integrally cast (84) into an assembled structure. (56
An all-blade steam gas turbine integrated engine, which is equipped with a device for a) being adiabatically provided to cool the combustion gas and to be driven by the output. 【請求項１４１】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の、磁気摩擦動力伝達
装置（１４）により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼蒸気ガスタービンにおいて、環状に
一体鋳造（８４）して組立構造とした内側タービン動翼
群（２０）の組立環状接続部付近に、水噴射手段（５６
ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該
出力で駆動する装置を具備したことを特徴とする全動翼
蒸気ガスタービン合体機関。141. An optimum rotation ratio of an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also functions as a friction pump (97) and that makes a combustion gas exhaust temperature close to −273 ° C. In a full-blade steam gas turbine having a water-repellent turbine blade, the water injection is performed in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) that is integrally cast (84) into an assembled structure. Means (56
An all-blade steam gas turbine integrated engine, characterized in that it is provided with a device for a) being heat-insulated to cool superheated steam and combustion gas and to be driven by the output. 【請求項１４２】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の、磁気摩擦動力伝達
装置（１４）により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼蒸気ガスタービンにおいて、環状に
一体鋳造（８４）して組立構造とした外側タービン動翼
群（１９）の組立環状接続部付近に、水噴射手段（５６
ａ）を断熱して設けて過熱蒸気や燃焼ガスを冷却し、該
出力で駆動する装置を具備したことを特徴とする全動翼
蒸気ガスタービン合体機関。142. The optimum rotation ratio between the outer shaft device and the inner shaft device that rotate in opposite directions by the magnetic friction power transmission device (14) that also functions as a friction pump (97) and that makes the combustion gas exhaust temperature close to −273 ° C. In an all-blade steam gas turbine that is coupled with a water-repellent turbine blade, water is injected near the assembled annular connection part of the outer turbine blade group (19) that is integrally cast (84) in an annular shape to form an assembled structure. Means (56
An all-blade steam gas turbine integrated engine, characterized in that it is provided with a device for a) being heat-insulated to cool superheated steam and combustion gas and to be driven by the output. 【請求項１４３】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造とした内側タービン動翼群
（２０）の組立環状接続部付近に、水噴射手段（５６
ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動
する装置を具備したことを特徴とする全動翼蒸気ガスタ
ービン合体機関。143. A total rotor blade having a water repellent turbine blade in which a combustion gas exhaust temperature is close to −273 ° C., an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. In the gas turbine, water injection means (56) is provided near the assembled annular connection portion of the inner turbine rotor blade group (20) that is integrally cast (84) in an annular shape to form an assembled structure.
An all-blade steam gas turbine integrated engine, which is equipped with a device for a) being adiabatically provided to cool the combustion gas and to be driven by the output. 【請求項１４４】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼ガスタービンにおいて、環状に一
体鋳造（８４）して組立構造とした外側タービン動翼群
（１９）の組立環状接続部付近に、水噴射手段（５６
ａ）を断熱して設けて燃焼ガスを冷却し、該出力で駆動
する装置を具備したことを特徴とする全動翼蒸気ガスタ
ービン合体機関。144. A total rotor blade having a water repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are combined at an optimum rotation ratio, and a combustion gas exhaust temperature approaches −273 ° C. In the gas turbine, the water injection means (56) is provided near the assembled annular connecting portion of the outer turbine blade group (19) that is integrally cast (84) in an annular shape to form an assembled structure.
An all-blade steam gas turbine integrated engine, which is equipped with a device for a) being adiabatically provided to cool the combustion gas and to be driven by the output. 【請求項１４５】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼蒸気ガスタービンにおいて、環状
に一体鋳造して組立構造とした内側タービン動翼群（２
０）の組立環状接続部付近に、水噴射手段（５６ａ）を
断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で
駆動する装置を具備したことを特徴とする全動翼蒸気ガ
スタービン合体機関。145. A total rotor blade having a water repellent turbine blade, in which a combustion gas exhaust temperature approaches −273 ° C., an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. In a steam gas turbine, an inner turbine rotor blade group (2
(0) A water jet means (56a) is provided in the vicinity of the assembled annular connection part so as to be heat-insulated to cool superheated steam or combustion gas, and a device for driving with this output is provided. Turbine united engine. 【請求項１４６】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼蒸気ガスタービンにおいて、環状
に一体鋳造して組立構造とした外側タービン動翼群（１
９）の組立環状接続部付近に、水噴射手段（５６ａ）を
断熱して設けて過熱蒸気や燃焼ガスを冷却し、該出力で
駆動する装置を具備したことを特徴とする全動翼蒸気ガ
スタービン合体機関。146. A total rotor blade having a water repellent turbine blade, in which a combustion gas exhaust temperature approaches −273 ° C., an outer shaft device and an inner shaft device rotating in opposite directions by a generator are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. In a steam gas turbine, an outer turbine rotor blade group (1
(9) A water jet means (56a) is provided near the assembled annular connection part so as to be heat-insulated to cool superheated steam and combustion gas, and a device for driving with this output is provided. Turbine united engine. 【請求項１４７】 復水器真空まで断熱膨張させる、摩
擦ポンプ（９７）兼用の磁気摩擦動力伝達装置（１４）
により互いに反対方向に回転する外側軸装置と内側軸装
置を最適回転比で結合し、撥水性タービン翼を具備した
全動翼蒸気タービンにおいて、環状に一体鋳造（８４）
して組立構造とした内側タービン動翼群（２０）の組立
環状接続部付近に、水噴射手段（５６ａ）を断熱して設
けたことを特徴とする全動翼蒸気ガスタービン合体機
関。147. A magnetic friction power transmission device (14) also serving as a friction pump (97), which adiabatically expands to a condenser vacuum.
The outer shaft device and the inner shaft device, which rotate in opposite directions to each other, are coupled with each other at an optimum rotation ratio, and in an all-blade steam turbine equipped with a water repellent turbine blade, they are integrally cast in an annular shape (84)
A water-jet injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) having the above-described assembled structure with heat insulation provided, and the all-blade steam gas turbine integrated engine is provided. 【請求項１４８】 復水器真空まで断熱膨張させる、摩
擦ポンプ（９７）兼用の磁気摩擦動力伝達装置（１４）
により互いに反対方向に回転する外側軸装置と内側軸装
置を最適回転比で結合し、撥水性タービン翼を具備した
全動翼蒸気タービンにおいて、環状に一体鋳造（８４）
して組立構造とした内側タービン動翼群（２０）の組立
環状接続部付近に、水噴射手段（５６ａ）を断熱して設
けて過熱蒸気を冷却し、該出力で駆動する装置を具備し
たことを特徴とする全動翼蒸気ガスタービン合体機関。148. A magnetic friction power transmission device (14) also serving as a friction pump (97), which adiabatically expands to a condenser vacuum.
The outer shaft device and the inner shaft device, which rotate in opposite directions to each other, are coupled with each other at an optimum rotation ratio, and in an all-blade steam turbine equipped with a water repellent turbine blade, they are integrally cast in an annular shape (84)
A water jet means (56a) is provided near the assembled annular connection part of the inner turbine rotor blade group (20) having an assembled structure by cooling so as to cool the superheated steam and drive by the output. An all-blade steam gas turbine integrated engine characterized by. 【請求項１４９】 復水器真空まで断熱膨張させる、摩
擦ポンプ（９７）兼用の磁気摩擦動力伝達装置（１４）
により互いに反対方向に回転する外側軸装置と内側軸装
置を最適回転比で結合し、撥水性タービン翼を具備した
全動翼蒸気タービンにおいて、環状に一体鋳造（８４）
して組立構造とした外側タービン動翼群（１９）の組立
環状接続部付近に、水噴射手段（５６ａ）を断熱して設
けたことを特徴とする全動翼蒸気ガスタービン合体機
関。149. A magnetic friction power transmission device (14) also serving as a friction pump (97), which adiabatically expands to a condenser vacuum.
The outer shaft device and the inner shaft device, which rotate in opposite directions to each other, are coupled with each other at an optimum rotation ratio, and in a full blade steam turbine equipped with a water repellent turbine blade, they are integrally cast in an annular shape (84)
A water-jet injection means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) having an assembled structure by heat-insulating the water-injection means (56a). 【請求項１５０】 復水器真空まで断熱膨張させる、摩
擦ポンプ（９７）兼用の磁気摩擦動力伝達装置（１４）
により互いに反対方向に回転する外側軸装置と内側軸装
置を最適回転比で結合し、撥水性タービン翼を具備した
全動翼蒸気タービンにおいて、環状に一体鋳造（８４）
して組立構造とした外側タービン動翼群（１９）の組立
環状接続部付近に、水噴射手段（５６ａ）を断熱して設
けて過熱蒸気を冷却し、該出力で駆動する装置を具備し
たことを特徴とする全動翼蒸気ガスタービン合体機関。150. A magnetic friction power transmission device (14) also serving as a friction pump (97), which adiabatically expands to a condenser vacuum.
The outer shaft device and the inner shaft device, which rotate in opposite directions to each other, are coupled with each other at an optimum rotation ratio, and in an all-blade steam turbine equipped with a water repellent turbine blade, they are integrally cast in an annular shape (84)
A water jet means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) having an assembled structure by heat insulation to cool the superheated steam and drive it with the output. An all-blade steam gas turbine integrated engine characterized by. 【請求項１５１】 復水器真空まで断熱膨張させる、発
電機により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気タービンにおいて、環状に一体鋳造して
組立構造とした内側タービン動翼群（２０）の組立環状
接続部付近に、水噴射手段（５６ａ）を断熱して設けた
ことを特徴とする全動翼蒸気ガスタービン合体機関。151. A full-blade steam turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which are adiabatically expanded to a condenser vacuum and rotate in opposite directions by a generator, are combined at an optimum rotation ratio. In all, the rotor blade steam gas is characterized in that the water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine blade group (20) integrally cast into an assembled structure. Turbine united engine. 【請求項１５２】 復水器真空まで断熱膨張させる、発
電機により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気タービンにおいて、環状に一体鋳造（８
４）して組立構造とした内側タービン動翼群（２０）の
組立環状接続部付近に、水噴射手段（５６ａ）を断熱し
て設けて過熱蒸気を冷却し、該出力で駆動する装置を具
備したことを特徴とする全動翼蒸気ガスタービン合体機
関。152. A full-blade steam turbine equipped with a water-repellent turbine blade, in which an outer shaft device and an inner shaft device, which are adiabatically expanded to a condenser vacuum and rotate in opposite directions by a generator, are combined at an optimum rotation ratio. In a ring,
4) A water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) having an assembled structure by heat insulation to cool the superheated steam and drive it with the output. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項１５３】 復水器真空まで断熱膨張させる、発
電機により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気タービンにおいて、環状に一体鋳造して
組立構造とした外側タービン動翼群（１９）の組立環状
接続部付近に、水噴射手段（５６ａ）を断熱して設けた
ことを特徴とする全動翼蒸気ガスタービン合体機関。153. A full-blade steam turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which are adiabatically expanded to a condenser vacuum and rotate in opposite directions by a generator, are combined at an optimum rotation ratio. In all, the rotor blade steam gas, wherein water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine rotor blade group (19) integrally cast into an assembled structure. Turbine united engine. 【請求項１５４】 復水器真空まで断熱膨張させる、発
電機により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気タービンにおいて、環状に一体鋳造（８
４）して組立構造とした外側タービン動翼群（１９）の
組立環状接続部付近に、水噴射手段（５６ａ）を断熱し
て設けて過熱蒸気を冷却し、該出力で駆動する装置を具
備したことを特徴とする全動翼蒸気ガスタービン合体機
関。154. A full-blade steam turbine equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which are adiabatically expanded to a condenser vacuum and rotate in opposite directions by a generator, are combined at an optimum rotation ratio. In a ring,
4) A water injection means (56a) is provided near the assembled annular connection part of the outer turbine blade group (19) having an assembled structure by heat insulation to cool the superheated steam and drive it with the output. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項１５５】 復水器真空まで断熱膨張させる、摩
擦ポンプ（９７）兼用の、磁気摩擦動力伝達装置（１
４）により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気ガスタービンにおいて、環状鋳造（８
４）して組立構造とした内側タービン動翼群（２０）の
組立環状接続部付近に、水噴射手段（５６ａ）を断熱し
て設けたことを特徴とする全動翼蒸気ガスタービン合体
機関。155. A magnetic friction power transmission device (1) also used as a friction pump (97) for adiabatically expanding to a condenser vacuum.
4) In an all-blade steam gas turbine equipped with a water-repellent turbine blade, the outer shaft device and the inner shaft device that rotate in opposite directions are coupled at an optimum rotation ratio by 4), and an annular casting (8
4) An all-blade steam-gas turbine integrated engine, characterized in that a water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) having an assembled structure. 【請求項１５６】 復水器真空まで断熱膨張させる、摩
擦ポンプ（９７）兼用の、磁気摩擦動力伝達装置（１
４）により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気ガスタービンにおいて、環状鋳造（８
４）して組立構造とした内側タービン動翼群（２０）の
組立環状接続部付近に、水噴射手段（５６ａ）を断熱し
て設けて過熱蒸気を冷却し、該出力で駆動する装置を具
備したことを特徴とする全動翼蒸気ガスタービン合体機
関。156. A magnetic friction power transmission device (1) also used as a friction pump (97) for adiabatically expanding to a condenser vacuum.
4) In an all-blade steam gas turbine equipped with a water-repellent turbine blade, the outer shaft device and the inner shaft device that rotate in opposite directions are coupled at an optimum rotation ratio by 4), and an annular casting (8
4) A water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) having an assembled structure by heat insulation to cool the superheated steam and drive it with the output. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項１５７】 復水器真空まで断熱膨張させる、摩
擦ポンプ（９７）兼用の、磁気摩擦動力伝達装置（１
４）により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気ガスタービンにおいて、環状鋳造（８
４）して組立構造とした外側タービン動翼群（１９）の
組立環状接続部付近に、水噴射手段（５６ａ）を断熱し
て設けたことを特徴とする全動翼蒸気ガスタービン合体
機関。157. A magnetic friction power transmission device (1) also used as a friction pump (97) for adiabatically expanding to a condenser vacuum.
4) In an all-blade steam gas turbine equipped with a water-repellent turbine blade, the outer shaft device and the inner shaft device that rotate in opposite directions are coupled at an optimum rotation ratio by 4), and an annular casting (8
4) An all-blade steam-gas turbine integrated engine, characterized in that a water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) having an assembled structure. 【請求項１５８】 復水器真空まで断熱膨張させる、摩
擦ポンプ（９７）兼用の、磁気摩擦動力伝達装置（１
４）により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気ガスタービンにおいて、環状鋳造（８
４）して組立構造とした外側タービン動翼群（１９）の
組立環状接続部付近に、水噴射手段（５６ａ）を断熱し
て設けて過熱蒸気を冷却し、該出力で駆動する装置を具
備したことを特徴とする全動翼蒸気ガスタービン合体機
関。158. A magnetic friction power transmission device (1) also serving as a friction pump (97), which adiabatically expands to a condenser vacuum.
4) In an all-blade steam gas turbine equipped with a water-repellent turbine blade, the outer shaft device and the inner shaft device that rotate in opposite directions are coupled at an optimum rotation ratio by 4), and an annular casting (8
4) A water injection means (56a) is provided near the assembled annular connection part of the outer turbine blade group (19) having an assembled structure by heat insulation to cool the superheated steam and drive it with the output. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項１５９】 復水器真空まで断熱膨張させる、発
電機により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気ガスタービンにおいて、環状鋳造（８
４）して組立構造とした内側タービン動翼群（２０）の
組立環状接続部付近に、水噴射手段（５６ａ）を断熱し
て設けたことを特徴とする全動翼蒸気ガスタービン合体
機関。159. Full-blade steam gas equipped with a water-repellent turbine blade by adiabatically expanding to a condenser vacuum, connecting an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, and having a water-repellent turbine blade. In the turbine, annular casting (8
4) An all-blade steam-gas turbine integrated engine, characterized in that a water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) having an assembled structure. 【請求項１６０】 復水器真空まで断熱膨張させる、発
電機により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気ガスタービンにおいて、環状鋳造（８
４）して組立構造とした内側タービン動翼群（２０）の
組立環状接続部付近に、水噴射手段（５６ａ）を断熱し
て設けて過熱蒸気を冷却し、該出力で駆動する装置を具
備したことを特徴とする全動翼蒸気ガスタービン合体機
関。160. A full rotor steam gas equipped with a water repellent turbine blade, wherein an outer shaft device and an inner shaft device, which are adiabatically expanded to a condenser vacuum and rotate in opposite directions by a generator, are combined at an optimum rotation ratio. In the turbine, annular casting (8
4) A water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the inner turbine rotor blade group (20) having an assembled structure by heat insulation to cool the superheated steam and drive it with the output. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項１６１】 復水器真空まで断熱膨張させる、発
電機により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気ガスタービンにおいて、環状鋳造（８
４）して組立構造とした外側タービン動翼群（１９）の
組立環状接続部付近に、水噴射手段（５６ａ）を断熱し
て設けたことを特徴とする全動翼蒸気ガスタービン合体
機関。161. Full-blade steam gas equipped with a water-repellent turbine blade by adiabatically expanding to a condenser vacuum, connecting an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio, and having a water-repellent turbine blade In the turbine, annular casting (8
4) An all-blade steam-gas turbine integrated engine, characterized in that a water injection means (56a) is provided in the vicinity of the assembled annular connection portion of the outer turbine blade group (19) having an assembled structure. 【請求項１６２】 復水器真空まで断熱膨張させる、発
電機により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼蒸気ガスタービンにおいて、環状鋳造（８
４）して組立構造とした外側タービン動翼群（１９）の
組立環状接続部付近に、水噴射手段（５６ａ）を断熱し
て設けて過熱蒸気を冷却し、該出力で駆動する装置を具
備したことを特徴とする全動翼蒸気ガスタービン合体機
関。162. Full-blade steam gas equipped with a water-repellent turbine blade by adiabatically expanding the condenser to a vacuum, connecting an outer shaft device and an inner shaft device rotating in opposite directions by a generator at an optimum rotation ratio In the turbine, annular casting (8
4) A water injection means (56a) is provided near the assembled annular connection part of the outer turbine blade group (19) having an assembled structure by heat insulation to cool the superheated steam and drive it with the output. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項１６３】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼ガスタービ
ンにおいて、有害物質を含む極低温燃焼ガスを核に水や
水蒸気を凝集して雹や水滴等とすることを特徴とする全
動翼蒸気ガスタービン合体機関。163. In a full-blade gas turbine equipped with a water-repellent turbine blade, which brings a combustion gas exhaust gas temperature close to -273 ° C., water or steam is condensed by using a cryogenic combustion gas containing a harmful substance as a core to hail or haze. A full-blade steam gas turbine combined engine characterized by water droplets. 【請求項１６４】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼蒸気ガスタ
ービンにおいて、石炭灰や有害物質を含む極低温燃焼ガ
スを核に水や水蒸気を凝集して雹や水滴等とすることを
特徴とする全動翼蒸気ガスタービン合体機関。164. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, which brings a combustion gas exhaust temperature close to -273 ° C., aggregates water and steam with a cryogenic combustion gas containing coal ash and harmful substances as a core. An all-blade steam gas turbine integrated engine characterized by being used as hail and water droplets. 【請求項１６５】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ兼用の、磁気摩擦動力伝達装置（１
４）により互いに反対方向に回転する外側軸装置と内側
軸装置を最適回転比で結合し、撥水性タービン翼を具備
した全動翼ガスタービンにおいて、有害物質を含む極低
温燃焼ガスを核に水や水蒸気を凝集して雹や水滴等とす
ることを特徴とする全動翼蒸気ガスタービン合体機関。165. A magnetic friction power transmission device (1) also serving as a friction pump, which brings a combustion gas exhaust gas temperature close to −273 ° C.
In 4), in an all-blade gas turbine equipped with a water-repellent turbine blade, an outer shaft device and an inner shaft device that rotate in opposite directions are coupled with each other at an optimum rotation ratio, and a cryogenic combustion gas containing harmful substances is used as a core for water. An all-blade steam gas turbine integrated engine characterized by aggregating steam and water vapor into hail and water droplets. 【請求項１６６】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の、磁気摩擦動力伝達
装置（１４）により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼蒸気ガスタービンにおいて、石炭灰
や有害物質を含む極低温燃焼ガスを核に水や水蒸気を凝
集して雹や水滴等とすることを特徴とする全動翼蒸気ガ
スタービン合体機関。166. An optimum rotation ratio of an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also functions as a friction pump (97) and that makes a combustion gas exhaust gas temperature close to −273 ° C. In a full-blade steam gas turbine equipped with a water-repellent turbine blade, it is characterized by using a cryogenic combustion gas containing coal ash and harmful substances as a core to agglomerate water and steam into hail, water droplets, etc. Combined full-blade steam gas turbine engine. 【請求項１６７】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼ガスタービンにおいて、有害物質
を含む極低温燃焼ガスを核に水や水蒸気を凝集して雹や
水滴等とすることを特徴とする全動翼蒸気ガスタービン
合体機関。167. A total rotor blade provided with a water repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are combined at an optimum rotation ratio, the combustion gas exhaust gas temperature approaching −273 ° C. In a gas turbine, an all-blade steam gas turbine integrated engine characterized by aggregating water and steam into hail and water droplets with a cryogenic combustion gas containing harmful substances as a core. 【請求項１６８】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼蒸気ガスタービンにおいて、石炭
灰や有害物質を含む極低温燃焼ガスを核に水や水蒸気を
凝集して雹や水滴等とすることを特徴とする全動翼蒸気
ガスタービン合体機関。168. A total rotor blade having a water-repellent turbine blade, in which a combustion gas exhaust temperature approaches -273 ° C., an outer shaft device and an inner shaft device that rotate in opposite directions by a generator are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. In a steam gas turbine, an all-blade steam gas turbine integrated engine characterized by agglomeration of water and steam into hail and water droplets with a cryogenic combustion gas containing coal ash and harmful substances as a core. 【請求項１６９】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼ガスタービ
ンにおいて、有害物質を含む極低温燃焼ガスを核に水や
水蒸気を凝集して雹や水滴等として分別し、分別した有
害物質を該合成溶解を促進する物質を含む水中に排出し
て、無害に近付けて放出することを特徴とする全動翼蒸
気ガスタービン合体機関。169. In a full-blade gas turbine equipped with a water-repellent turbine blade, which brings a combustion gas exhaust gas temperature close to -273 ° C., water or steam is condensed by using a cryogenic combustion gas containing a harmful substance as a nucleus to form a hail or hail. An all-blade steam-gas turbine integrated engine, characterized in that it is separated into water droplets and the like, and the separated harmful substances are discharged into water containing a substance that promotes the synthetic dissolution, and are discharged in a harmless manner. 【請求項１７０】 燃焼ガス排気温度を−２７３℃に近
付ける、撥水性タービン翼を具備した全動翼蒸気ガスタ
ービンにおいて、有害物質を含む極低温燃焼ガスを核に
水や水蒸気を凝集して雹や水滴等として分別し、分別し
た有害物質を該合成溶解を促進する物質を含む水中に排
出して、無害に近付けて放出することを特徴とする全動
翼蒸気ガスタービン合体機関。170. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, which brings a combustion gas exhaust gas temperature close to -273 ° C., water and steam are condensed by using a cryogenic combustion gas containing a harmful substance as a core to hail. An all- moving blade steam gas turbine integrated engine, characterized in that it is separated into water, water droplets, etc., and the separated harmful substances are discharged into water containing a substance that promotes the synthetic dissolution, and are discharged in a harmless manner. 【請求項１７１】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の、磁気摩擦動力伝達
装置（１４）により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼ガスタービンにおいて、有害物質を
含む極低温燃焼ガスを核に水や水蒸気を凝集して雹や水
滴等として分別し、分別した有害物質を該合成溶解を促
進する物質を含む水中に排出して、無害に近付けて放出
することを特徴とする全動翼蒸気ガスタービン合体機
関。171. An optimum rotation ratio of an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also serves as a friction pump (97) and that makes a combustion gas exhaust gas temperature close to -273 ° C. In an all-blade gas turbine equipped with a water-repellent turbine blade, the cryogenic combustion gas containing harmful substances is condensed into water and steam by the core to separate them as hail and water droplets, and the separated harmful substances are An all-blade steam gas turbine integrated engine, which discharges into water containing a substance that promotes synthetic dissolution, and releases it in a harmless manner. 【請求項１７２】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の、磁気摩擦動力伝達
装置（１４）により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼蒸気ガスタービンにおいて、有害物
質を含む極低温燃焼ガスを核に水や水蒸気を凝集して雹
や水滴等として分別し、分別した有害物質を該合成溶解
を促進する物質を含む水中に排出して、無害に近付けて
放出することを特徴とする全動翼蒸気ガスタービン合体
機関。172. An optimum rotation ratio of an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also serves as a friction pump (97) and that makes a combustion gas exhaust temperature close to −273 ° C. In an all-blade steam gas turbine equipped with a water-repellent turbine blade, the cryogenic combustion gas containing harmful substances is aggregated into water and water vapor to separate it into hail and water droplets. A full-blade steam gas turbine integrated engine, which is discharged into water containing a substance that promotes the synthetic dissolution, and is discharged in a harmless manner. 【請求項１７３】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼ガスタービンにおいて、有害物質
を含む極低温燃焼ガスを核に水や水蒸気を凝集して雹や
水滴等として分別し、分別した有害物質を該合成溶解を
促進する物質を含む水中に排出して、無害に近付けて放
出することを特徴とする全動翼蒸気ガスタービン合体機
関。173. A total rotor blade having a water repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are combined at an optimum rotation ratio, the combustion gas exhaust gas temperature approaching −273 ° C. In a gas turbine, cryogenic combustion gas containing a harmful substance is separated into water and water vapor by aggregating water and steam into a hail, water droplets, etc., and the separated harmful substance is discharged into water containing a substance that promotes the synthetic dissolution, A full-blade steam gas turbine integrated engine characterized in that it is emitted in the vicinity of harmless. 【請求項１７４】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼蒸気ガスタービンにおいて、有害
物質を含む極低温燃焼ガスを核に水や水蒸気を凝集して
雹や水滴等として分別し、分別した有害物質を該合成溶
解を促進する物質を含む水中に排出して、無害に近付け
て放出することを特徴とする全動翼蒸気ガスタービン合
体機関。174. A total rotor blade provided with a water repellent turbine blade, in which an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are coupled at an optimum rotation ratio, and a combustion gas exhaust gas temperature approaches −273 ° C. In a steam gas turbine, cryogenic combustion gas containing harmful substances is condensed into nuclei to separate water and steam into hail, water drops, etc., and the separated harmful substances are discharged into water containing a substance that promotes the synthetic dissolution. , A full-blade steam gas turbine integrated engine characterized by being emitted in a harmless manner. 【請求項１７５】 燃焼ガス排気温度を−２７３℃に近
付ける、、撥水性タービン翼を具備し全動翼ガスタービ
ンにおいて、有害物質を含む極低温燃焼ガスを核に水や
水蒸気を凝集して雹や水滴等として分別し、該出力で駆
動する装置を具備したことを特徴とする全動翼蒸気ガス
タービン合体機関。175. In an all-blade gas turbine equipped with a water-repellent turbine blade that brings the exhaust temperature of the combustion gas close to -273 ° C., water or steam is aggregated with a cryogenic combustion gas containing a harmful substance as a core to form a hail. An all-blade steam gas turbine integrated engine equipped with a device that separates water, water droplets, etc., and drives with the output. 【請求項１７６】 燃焼ガス排気温度を−２７３℃に近
付ける、、撥水性タービン翼を具備し全動翼蒸気ガスタ
ービンにおいて、有害物質を含む極低温燃焼ガスを核に
水や水蒸気を凝集して雹や水滴等として分別し、該出力
で駆動する装置を具備したことを特徴とする全動翼蒸気
ガスタービン合体機関。176. In a full-blade steam gas turbine equipped with a water-repellent turbine blade for bringing a combustion gas exhaust temperature close to -273 ° C., water or steam is condensed by using a cryogenic combustion gas containing a harmful substance as a core. An all-blade steam gas turbine integrated engine equipped with a device that separates into hail, water droplets, etc., and drives with the output. 【請求項１７７】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の、磁気摩擦動力伝達
装置（１４）により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼ガスタービンにおいて、有害物質を
含む極低温燃焼ガスを核に水や水蒸気を凝集して雹や水
滴等として分別し、該出力で駆動する装置を具備したこ
とを特徴とする全動翼蒸気ガスタービン合体機関。177. An optimum rotation ratio between an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also functions as a friction pump (97) and that makes a combustion gas exhaust gas temperature close to −273 ° C. In a full-blade gas turbine equipped with a water-repellent turbine blade, a device that drives ultra-low temperature combustion gas containing harmful substances by condensing water and steam into hail, water droplets, etc. An all-blade steam gas turbine integrated engine, characterized by comprising: 【請求項１７８】 燃焼ガス排気温度を−２７３℃に近
付ける、摩擦ポンプ（９７）兼用の、磁気摩擦動力伝達
装置（１４）により互いに反対方向に回転する外側軸装
置と内側軸装置を最適回転比で結合し、撥水性タービン
翼を具備した全動翼蒸気ガスタービンにおいて、有害物
質を含む極低温燃焼ガスを核に水や水蒸気を凝集して雹
や水滴等として分別し、該出力で駆動する装置を具備し
たことを特徴とする全動翼蒸気ガスタービン合体機関。178. An optimum rotation ratio of an outer shaft device and an inner shaft device that rotate in opposite directions by a magnetic friction power transmission device (14) that also serves as a friction pump (97) and that makes a combustion gas exhaust temperature close to -273 ° C. In a full-blade steam gas turbine equipped with a water-repellent turbine blade, the cryogenic combustion gas containing harmful substances is condensed into nuclei to separate water and steam into hail, water droplets, etc., and driven by the output. An all-blade steam gas turbine integrated engine equipped with a device. 【請求項１７９】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼ガスタービンにおいて、有害物質
を含む極低温燃焼ガスを核に水や水蒸気を凝集して雹や
水滴等として分別し、該出力で駆動する装置を具備した
ことを特徴とする全動翼蒸気ガスタービン合体機関。179. A total rotor blade provided with a water repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are combined at an optimum rotation ratio, the combustion gas exhaust gas temperature approaching -273 ° C. In a gas turbine, an all-blade steam gas turbine is equipped with a device that drives a cryogenic combustion gas containing a harmful substance into a core by condensing water or steam into hail, water droplets, etc., and driving with the output. Coalescing agency. 【請求項１８０】 燃焼ガス排気温度を−２７３℃に近
付ける、発電機により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼蒸気ガスタービンにおいて、有害
物質を含む極低温燃焼ガスを核に水や水蒸気を凝集して
雹や水滴等として分別し、該出力で駆動する装置を具備
したことを特徴とする全動翼蒸気ガスタービン合体機
関。180. A total rotor blade having a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which rotate in opposite directions by a generator, are coupled at an optimum rotation ratio and a combustion gas exhaust gas temperature approaches −273 ° C. In a steam gas turbine, a cryogenic combustion gas containing a harmful substance is condensed into water as a nucleus to separate water and steam into fractions such as hail and water droplets, and is equipped with a device driven by the output. Turbine united engine. 【請求項１８１】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンの内側軸装
置を中空として、霧吹きの原理９１を利用して前方の空
気を吸引噴射することを特徴とする全動翼蒸気ガスター
ビン合体機関。181. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A full-blade steam gas turbine integrated engine, characterized in that a hollow inner shaft device of the full-blade gas turbine is used to suck and inject forward air by utilizing a spraying principle 91. 【請求項１８２】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの内側
軸装置を中空として、霧吹きの原理９１を利用して前方
の空気を吸引噴射することを特徴とする全動翼蒸気ガス
タービン合体機関。182. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. An all-blade steam gas turbine integrated engine, characterized in that a hollow inner shaft device of the all-blade steam gas turbine is used to suck and inject forward air by utilizing a spraying principle 91. 【請求項１８３】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンの内側軸装
置を中空として、霧吹きの原理９１を利用して前方の空
気を吸引噴射することを特徴とする全動翼蒸気ガスター
ビン合体機関。183. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A full-blade steam gas turbine integrated engine, characterized in that a hollow inner shaft device of the full-blade steam turbine is used to suck and inject forward air by utilizing a spraying principle 91. 【請求項１８４】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンの燃焼器兼
熱交換器出口に、燃焼ガス取出口（８８）を設けたこと
を特徴とする全動翼蒸気ガスタービン合体機関。184. An outer shaft device and an inner shaft device, which also serve as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. An all-blade steam gas turbine integrated engine, characterized in that a combustion gas outlet (88) is provided at the combustor-heat exchanger outlet of the all-blade gas turbine. 【請求項１８５】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの燃焼
器兼熱交換器出口に、燃焼ガス取出口（８８）を設けた
ことを特徴とする全動翼蒸気ガスタービン合体機関。185. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A full-blade steam gas turbine integrated engine, characterized in that a combustion gas outlet (88) is provided at a combustor-heat exchanger outlet of the full-blade steam gas turbine. 【請求項１８６】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンの燃焼器兼
熱交換器出口に、燃焼ガス取出口（８８）を設けたこと
を特徴とする全動翼蒸気ガスタービン合体機関。186. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A full-blade steam gas turbine integrated engine, characterized in that a combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of the full-blade steam turbine. 【請求項１８７】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンの燃焼器兼
熱交換器出口に、燃焼ガス取出口（８８）を設けて、マ
イクロガスタービンを駆動することを特徴とする全動翼
蒸気ガスタービン合体機関。187. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A full-blade steam gas turbine integrated engine, characterized in that a combustion gas outlet (88) is provided at a combustor-heat exchanger outlet of a full-blade gas turbine to drive a micro gas turbine. 【請求項１８８】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの燃焼
器兼熱交換器出口に、燃焼ガス取出口（８８）を設け
て、マイクロガスタービンを駆動することを特徴とする
全動翼蒸気ガスタービン合体機関。188. An outer shaft device and an inner shaft device, which also serve as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. An all-blade steam gas turbine integrated engine, characterized in that a combustion gas outlet (88) is provided at a combustor / heat exchanger outlet of the all-blade steam gas turbine to drive a micro gas turbine. 【請求項１８９】 摩擦ポンプ兼用の、磁気摩擦動力伝
達装置（１４）により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼ガスタービンに於いて、霧吹きの
原理（９１）を利用して１以上複数の特殊装置（９２）
より過熱蒸気を噴射し、前方の空気を吸引して噴射する
ことを特徴とする全動翼蒸気ガスタービン合体機関。189. A total rotor blade equipped with a water-repellent turbine blade, wherein an outer shaft device and an inner shaft device, which also function as a friction pump and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio. In the gas turbine, one or more special devices (92) using the principle of atomization (91)
A full-blade steam gas turbine integrated engine characterized by injecting more superheated steam and sucking and injecting air in front. 【請求項１９０】 摩擦ポンプ兼用の、磁気摩擦動力伝
達装置（１４）により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼蒸気ガスタービンに於いて、霧吹
きの原理（９１）を利用して１以上複数の特殊装置（９
２）より過熱蒸気を噴射し、前方の空気を吸引して噴射
することを特徴とする全動翼蒸気ガスタービン合体機
関。190. A total rotor blade equipped with a water repellent turbine blade, wherein an outer shaft device and an inner shaft device, which also function as a friction pump and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio. In a steam gas turbine, one or more special devices (9
2) An all-blade steam gas turbine integrated engine characterized by injecting superheated steam from 2) and sucking and injecting air in the front. 【請求項１９１】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの燃焼
器兼熱交換器出口に、燃焼ガス取出口（８８）を設け
て、霧吹きの原理（９１）を利用して１以上複数の特殊
装置（９２）より燃焼ガスを噴射し、前方の空気を吸引
して噴射することを特徴とする全動翼蒸気ガスタービン
合体機関。191. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of the all-blade steam gas turbine, and the combustion gas is supplied from one or more special devices (92) using the atomization principle (91). An all-blade steam-gas turbine combined engine, which injects and sucks air in the front to inject it. 【請求項１９２】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンの燃焼器兼
熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧
吹きの原理（９１）を利用して１以上複数の特殊装置
（９２）より燃焼ガスを噴射し、前方の空気を吸引して
噴射することを特徴とする全動翼蒸気ガスタービン合体
機関。192. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of the all-blade steam turbine, and the combustion gas is injected from one or more special devices (92) by using the atomization principle (91). However, a full moving blade steam gas turbine integrated engine is characterized in that it sucks and injects the air in front. 【請求項１９３】 摩擦ポンプ兼用の、磁気摩擦動力伝
達装置（１４）により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼ガスタービンに於いて、霧吹きの
原理（９１）を利用して１以上複数の水噴射装置（９
３）より過熱蒸気を噴射し、前方の水を吸引して噴射す
ることを特徴とする全動翼蒸気ガスタービン合体機関。193. A total rotor blade equipped with a water repellent turbine blade, wherein an outer shaft device and an inner shaft device, which also function as a friction pump and rotate in mutually opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio. In a gas turbine, one or more water injection devices (9
3) A super moving steam turbine integrated engine characterized by injecting superheated steam from 3) and sucking and injecting water in front. 【請求項１９４】 摩擦ポンプ兼用の、磁気摩擦動力伝
達装置（１４）により互いに反対方向に回転する外側軸
装置と内側軸装置を最適回転比で結合し、撥水性タービ
ン翼を具備した全動翼蒸気ガスタービンに於いて、霧吹
きの原理（９１）を利用して１以上複数の水噴射装置
（９３）より過熱蒸気を噴射し、前方の水を吸引して噴
射することを特徴とする全動翼蒸気ガスタービン合体機
関。194. A total rotor blade equipped with a water repellent turbine blade, wherein an outer shaft device and an inner shaft device, which also function as a friction pump, and which rotate in opposite directions by a magnetic friction power transmission device (14) are coupled at an optimum rotation ratio. In a steam gas turbine, one or more water injection devices (93) are used to inject superheated steam by utilizing the atomization principle (91), and water in front is sucked and injected. Wing steam gas turbine combined engine. 【請求項１９５】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの燃焼
器兼熱交換器出口に、燃焼ガス取出口（８８）を設け
て、霧吹きの原理（９１）を利用して１以上複数の水噴
射装置（９３）より燃焼ガスを噴射し、前方の水を吸引
して噴射することを特徴とする全動翼蒸気ガスタービン
合体機関。195. An outer shaft device and an inner shaft device, which also serve as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of the all-blade steam gas turbine, and the combustion gas is supplied from one or more water injection devices (93) using the atomization principle (91). An all-blade steam-gas turbine combined engine, which injects water, and sucks and injects water in front. 【請求項１９６】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンの燃焼器兼
熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧
吹きの原理（９１）を利用して１以上複数の水噴射装置
（９３）より燃焼ガスを噴射し、前方の水を吸引して噴
射することを特徴とする全動翼蒸気ガスタービン合体機
関。196. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of an all-blade steam turbine, and combustion gas is supplied from one or more water injection devices (93) by utilizing the atomization principle (91). An all-blade steam-gas turbine combined engine that injects water and sucks water in front of it to inject it. 【請求項１９７】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの燃焼
器兼熱交換器出口に、燃焼ガス取出口（８８）を設け
て、霧吹きの原理（９１）を利用して夫々の１以上複数
の水噴射装置（９３）より過熱蒸気及び燃焼ガスを噴射
し、前方の水を吸引して噴射することを特徴とする全動
翼蒸気ガスタービン合体機関。197. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are connected at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of the full-blade steam gas turbine, and the principle of atomization (91) is used to make each one or more water injection devices (93) An all- moving blade steam gas turbine integrated engine characterized by injecting superheated steam and combustion gas, and sucking in and injecting water in front. 【請求項１９８】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンの燃焼器兼
熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧
吹きの原理（９１）を利用して夫々の１以上複数の水噴
射装置（９３）より過熱蒸気及び燃焼ガスを噴射し、前
方の水を吸引して噴射することを特徴とする全動翼蒸気
ガスタービン合体機関。198. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of a full-blade steam turbine, and superheated by one or more water injection devices (93) using the atomization principle (91). A full-blade steam-gas turbine integrated engine characterized by injecting steam and combustion gas and sucking in and ejecting water in front. 【請求項１９９】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの燃焼
器兼熱交換器出口に、燃焼ガス取出口（８８）を設け
て、霧吹きの原理（９１）を利用して夫々の１以上複数
の特殊装置（９２）より過熱蒸気及び燃焼ガスを噴射
し、前方の空気を吸引して噴射することを特徴とする全
動翼蒸気ガスタービン合体機関。199. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of an all-blade steam gas turbine to superheat from one or more special devices (92) using the atomization principle (91). An all-blade steam gas turbine integrated engine characterized by injecting steam and combustion gas and sucking in and injecting air in front. 【請求項２００】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンの燃焼器兼
熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧
吹きの原理（９１）を利用して夫々の１以上複数の特殊
装置（９２）より過熱蒸気及び燃焼ガスを噴射し、前方
の空気を吸引して噴射することを特徴とする全動翼蒸気
ガスタービン合体機関。200. An outer shaft device and an inner shaft device, which also serve as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of an all-blade steam turbine, and superheated steam is generated from each of one or more special devices (92) by utilizing the atomization principle (91). And a combustion engine for injecting combustion gas, and sucking and injecting air in front of the combustion engine. 【請求項２０１】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンに於いて、
霧吹きの原理（９１）を利用して１以上複数の特殊装置
（９２）より過熱蒸気を噴射し、前方の空気を吸引して
噴射推進し、該出力で駆動する装置を具備したことを特
徴とする全動翼蒸気ガスタービン合体機関。201. A magnetic repulsive power transmission device (14), which also serves as a friction pump (97), connects an outer shaft device and an inner shaft device that rotate in opposite directions to each other at an optimum rotation ratio, and comprises a water repellent turbine blade. In a full-blade gas turbine,
A device for injecting superheated steam from one or more special devices (92) utilizing the principle of atomization (91), sucking forward air to inject and propel it, and driving it with the output is provided. Combined full-blade steam gas turbine engine. 【請求項２０２】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンに於い
て、霧吹きの原理（９１）を利用して１以上複数の特殊
装置（９２）より過熱蒸気を噴射し、前方の空気を吸引
して噴射推進し、該出力で駆動する装置を具備したこと
を特徴とする全動翼蒸気ガスタービン合体機関。202. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. In an all-blade steam gas turbine, superheated steam is injected from one or more special devices (92) by utilizing the principle of atomization (91), air in front is sucked and propelled, and at this output. An all-blade steam gas turbine integrated engine having a driving device. 【請求項２０３】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの燃焼
器兼熱交換器出口に、燃焼ガス取出口（８８）を設け
て、霧吹きの原理（９１）を利用して１以上複数の特殊
装置（９２）より燃焼ガスを噴射し、前方の空気を吸引
して噴射推進し、該出力で駆動する装置を具備したこと
を特徴とする全動翼蒸気ガスタービン合体機関。203. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of the all-blade steam gas turbine, and the combustion gas is supplied from one or more special devices (92) using the atomization principle (91). An all-blade steam gas turbine integrated engine comprising a device for injecting, sucking air in the front, injecting and propelling, and driving with the output. 【請求項２０４】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンの燃焼器兼
熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧
吹きの原理（９１）を利用して１以上複数の特殊装置
（９２）より燃焼ガスを噴射し、前方の空気を吸引して
噴射推進し、該出力で駆動する装置を具備したことを特
徴とする全動翼蒸気ガスタービン合体機関。204. A water-repellent turbine blade is provided, wherein an outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of the all-blade steam turbine, and the combustion gas is injected from one or more special devices (92) by using the atomization principle (91). However, the all-blade steam gas turbine integrated engine is equipped with a device that sucks in the air in the front, injects and propels it, and drives it with the output. 【請求項２０５】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼ガスタービンに於いて、
霧吹きの原理（９１）を利用して１以上複数の水噴射装
置（９３）より過熱蒸気を噴射し、前方の水を吸引して
噴射推進し、該出力で駆動する装置を具備したことを特
徴とする全動翼蒸気ガスタービン合体機関。205. A magnetic repulsive power transmission device (14), which also serves as a friction pump (97), connects an outer shaft device and an inner shaft device that rotate in opposite directions to each other at an optimum rotation ratio, and comprises a water repellent turbine blade. In a full-blade gas turbine,
It is equipped with a device for injecting superheated steam from one or more water injection devices (93) by using the principle of atomization (91), sucking water in front of the device, propelling it, and driving it with the output. Combined full-blade steam gas turbine engine. 【請求項２０６】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンに於い
て、霧吹きの原理（９１）を利用して１以上複数の水噴
射装置（９３）より過熱蒸気を噴射し、前方の水を吸引
して噴射推進し、該出力で駆動する装置を具備したこと
を特徴とする全動翼蒸気ガスタービン合体機関。206. A water-repellent turbine blade is provided, wherein an outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio. In an all-blade steam gas turbine, superheated steam is injected from one or more water injection devices (93) by utilizing the atomization principle (91), water in front is sucked and propelled, and the output An all-blade steam gas turbine integrated engine, characterized in that it is equipped with a device driven by. 【請求項２０７】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの燃焼
器兼熱交換器出口に、燃焼ガス取出口（８８）を設け
て、霧吹きの原理（９１）を利用して１以上複数の水噴
射装置（９３）より燃焼ガスを噴射し、前方の水を吸引
して噴射推進し、該出力で駆動する装置を具備したこと
を特徴とする全動翼蒸気ガスタービン合体機関。207. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of the all-blade steam gas turbine, and the combustion gas is supplied from one or more water injection devices (93) using the atomization principle (91). A steam turbine integrated unit with all moving blades, comprising: 【請求項２０８】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンの燃焼器兼
熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧
吹きの原理（９１）を利用して１以上複数の水噴射装置
（９３）より燃焼ガスを噴射し、前方の水を吸引して噴
射推進し、該出力で駆動する装置を具備したことを特徴
とする全動翼蒸気ガスタービン合体機関。208. A water repellent turbine blade is provided, wherein an outer shaft device and an inner shaft device, which also serve as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of an all-blade steam turbine, and combustion gas is supplied from one or more water injection devices (93) by utilizing the atomization principle (91). An all-blade steam-gas turbine integrated engine comprising a device for injecting, sucking water in front of it, injecting and propelling it, and driving it by the output. 【請求項２０９】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの燃焼
器兼熱交換器出口に、燃焼ガス取出口（８８）を設け
て、霧吹きの原理（９１）を利用して夫々の１以上複数
の水噴射装置（９３）より過熱蒸気及び燃焼ガスを噴射
し、前方の水を吸引して噴射推進し、該出力で駆動する
装置を具備したことを特徴とする全動翼蒸気ガスタービ
ン合体機関。209. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are connected at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of the full-blade steam gas turbine, and the principle of atomization (91) is used to make each one or more water injection devices (93) An all-blade steam-gas turbine integrated engine, comprising a device for injecting superheated steam and combustion gas, sucking in water in front of it, injecting and propelling it, and driving it by the output. 【請求項２１０】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンの燃焼器兼
熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧
吹きの原理（９１）を利用して夫々の１以上複数の水噴
射装置（９３）より過熱蒸気及び燃焼ガスを噴射し、前
方の水を吸引して噴射推進し、該出力で駆動する装置を
具備したことを特徴とする全動翼蒸気ガスタービン合体
機関。210. A water repellent turbine blade is provided, wherein an outer shaft device and an inner shaft device, which also serve as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of a full-blade steam turbine, and superheated by one or more water injection devices (93) using the atomization principle (91). An all-blade steam-gas turbine integrated engine comprising a device for injecting steam and combustion gas, sucking water in the front side, injecting and propelling the water, and driving with the output. 【請求項２１１】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気ガスタービンの燃焼
器兼熱交換器出口に、燃焼ガス取出口（８８）を設け
て、霧吹きの原理（９１）を利用して夫々の１以上複数
の特殊装置（９２）より過熱蒸気及び燃焼ガスを噴射
し、前方の空気を吸引して噴射推進し、該出力で駆動す
る装置を具備したことを特徴とする全動翼蒸気ガスター
ビン合体機関。211. An outer shaft device and an inner shaft device, which also serve as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of an all-blade steam gas turbine to superheat from one or more special devices (92) using the atomization principle (91). An all-blade steam gas turbine integrated engine comprising a device for injecting steam and combustion gas, sucking forward air to inject and propel it, and driving with the output. 【請求項２１２】 摩擦ポンプ（９７）兼用の、磁気摩
擦動力伝達装置（１４）により互いに反対方向に回転す
る外側軸装置と内側軸装置を最適回転比で結合し、撥水
性タービン翼を具備した全動翼蒸気タービンの燃焼器兼
熱交換器出口に、燃焼ガス取出口（８８）を設けて、霧
吹きの原理（９１）を利用して夫々の１以上複数の特殊
装置（９２）より過熱蒸気及び燃焼ガスを噴射し、前方
の空気を吸引して噴射推進し、該出力で駆動する装置を
具備したことを特徴とする全動翼蒸気ガスタービン合体
機関。212. An outer shaft device and an inner shaft device, which also function as a friction pump (97) and rotate in opposite directions by a magnetic friction power transmission device (14), are coupled at an optimum rotation ratio, and a water repellent turbine blade is provided. A combustion gas outlet (88) is provided at the combustor / heat exchanger outlet of an all-blade steam turbine, and superheated steam is generated from each of one or more special devices (92) by utilizing the atomization principle (91). And a device for injecting combustion gas, sucking forward air, injecting and propelling the same, and driving with the output, the all-blade steam gas turbine integrated engine. 【請求項２１３】 撥水性タービン翼を具備した全動翼
ガスタービンの燃焼器兼熱交換器（４）において、霧吹
きの原理（９１）を利用して１以上複数の特殊装置（９
２）より過熱蒸気を噴射し、前方の空気を吸引して噴射
することを特徴とする全動翼蒸気ガスタービン合体機
関。213. In a combustor / heat exchanger (4) of an all-blade gas turbine equipped with a water-repellent turbine blade, one or more special devices (9) utilizing the atomization principle (91).
2) An all-blade steam gas turbine integrated engine characterized by injecting superheated steam from 2) and sucking and injecting air in the front. 【請求項２１４】 撥水性タービン翼を具備した全動翼
ガスタービンの燃焼器兼熱交換器（４）において、霧吹
きの原理（９１）を利用して１以上複数の水噴射装置
（９３）より過熱蒸気を噴射し、前方の水を吸引して噴
射することを特徴とする全動翼蒸気ガスタービン合体機
関。214. In a combustor / heat exchanger (4) of an all-blade gas turbine equipped with water repellent turbine blades, one or more water injection devices (93) utilizing the principle of atomization (91). An all-blade steam-gas turbine integrated engine characterized by injecting superheated steam and sucking water in front of it to inject it. 【請求項２１５】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
霧吹きの原理（９１）を利用して１以上複数の特殊装置
（９２）より過熱蒸気を噴射し、前方の空気を吸引して
噴射することを特徴とする全動翼蒸気ガスタービン合体
機関。215. A combustor and heat exchanger (4) for an all-blade steam gas turbine equipped with a water-repellent turbine blade,
A full-blade steam-gas turbine integrated engine characterized by injecting superheated steam from one or more special devices (92) by utilizing the principle of atomization (91), and sucking and injecting air in front. 【請求項２１６】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
霧吹きの原理（９１）を利用して１以上複数の水噴射装
置（９３）より過熱蒸気を噴射し、前方の水を吸引して
噴射することを特徴とする全動翼蒸気ガスタービン合体
機関。216. A combustor and heat exchanger (4) for a full moving blade steam gas turbine, comprising a water repellent turbine blade,
A full-blade steam-gas turbine integrated engine characterized by injecting superheated steam from one or more water injection devices (93) by using the atomization principle (91), and sucking and injecting front water. 【請求項２１７】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹
きの原理（９１）を利用して夫々の１以上複数の特殊装
置（９２）より過熱蒸気及び燃焼ガスを噴射し、前方の
空気を吸引して噴射することを特徴とする全動翼蒸気ガ
スタービン合体機関。217. A combustor and heat exchanger (4) for an all-blade steam gas turbine equipped with a water-repellent turbine blade,
A combustion gas outlet (88) is provided at the combustion gas outlet, and superheated steam and combustion gas are injected from each of one or more special devices (92) by utilizing the principle of atomization (91), and the air in front is An all-blade steam gas turbine integrated engine characterized by suction and injection. 【請求項２１８】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹
きの原理（９１）を利用して夫々の１以上複数の水噴射
装置（９３）より過熱蒸気及び燃焼ガスを噴射し、前方
の水を吸引して噴射することを特徴とする全動翼蒸気ガ
スタービン合体機関。218. A combustor and heat exchanger (4) for an all-blade steam gas turbine equipped with a water-repellent turbine blade,
A combustion gas outlet (88) is provided at the combustion gas outlet, and superheated steam and combustion gas are injected from each of one or more water injection devices (93) by utilizing the principle of atomization (91), and water in front is discharged. An all-blade steam-gas turbine integrated engine characterized by sucking and injecting. 【請求項２１９】 撥水性タービン翼を具備した全動翼
蒸気タービンの燃焼器兼熱交換器（４）において、燃焼
ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの
原理（９１）を利用して夫々の１以上複数の特殊装置
（９２）より過熱蒸気及び燃焼ガスを噴射し、前方の空
気を吸引して噴射することを特徴とする全動翼蒸気ガス
タービン合体機関。219. In a combustor / heat exchanger (4) of an all-blade steam turbine equipped with a water repellent turbine blade, a combustion gas outlet (88) is provided at a combustion gas outlet, and a spraying principle (91) is provided. A superfluid blade steam gas turbine integrated engine, characterized in that superheated steam and combustion gas are injected from each of one or more special devices (92) using the above, and front air is sucked and injected. 【請求項２２０】 撥水性タービン翼を具備した全動翼
蒸気タービンの燃焼器兼熱交換器（４）において、燃焼
ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの
原理（９１）を利用して夫々の１以上複数の水噴射装置
（９３）より過熱蒸気及び燃焼ガスを噴射し、前方の水
を吸引して噴射することを特徴とする全動翼蒸気ガスタ
ービン合体機関。220. In a combustor / heat exchanger (4) of an all-blade steam turbine equipped with a water repellent turbine blade, a combustion gas outlet (88) is provided at a combustion gas outlet, and a spraying principle (91) is provided. Is used to inject superheated steam and combustion gas from one or more water injecting devices (93) respectively, and suck water in front to inject the water, thereby combining all-blade steam gas turbines. 【請求項２２１】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹
きの原理（９１）を利用して１以上複数の特殊装置（９
２）より燃焼ガスを噴射し、前方の空気を吸引して噴射
することを特徴とする全動翼蒸気ガスタービン合体機
関。221. A combustor and heat exchanger (4) for an all-blade steam gas turbine equipped with a water-repellent turbine blade,
A combustion gas outlet (88) is provided at the combustion gas outlet to utilize one or more special devices (9) by utilizing the atomization principle (91).
(2) A full-blade steam gas turbine integrated engine characterized by injecting combustion gas from (2) and sucking and injecting air ahead. 【請求項２２２】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹
きの原理（９１）を利用して１以上複数の水噴射装置
（９３）より燃焼ガスを噴射し、前方の水を吸引して噴
射することを特徴とする全動翼蒸気ガスタービン合体機
関。222. A combustor and heat exchanger (4) for an all-blade steam gas turbine equipped with a water-repellent turbine blade,
A combustion gas outlet (88) is provided at the combustion gas outlet, and the combustion gas is injected from one or more water injection devices (93) by utilizing the atomization principle (91), and water in front is sucked and injected. An all-blade steam gas turbine integrated engine characterized by 【請求項２２３】 撥水性タービン翼を具備した全動翼
蒸気タービンの燃焼器兼熱交換器（４）において、燃焼
ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの
原理（９１）を利用して１以上複数の特殊装置（９２）
より燃焼ガスを噴射し、前方の空気を吸引して噴射する
ことを特徴とする全動翼蒸気ガスタービン合体機関。223. In a combustor and heat exchanger (4) of an all-blade steam turbine equipped with a water repellent turbine blade, a combustion gas outlet (88) is provided at a combustion gas outlet, and a spraying principle (91). One or more special devices using (92)
A full-blade steam gas turbine integrated engine characterized by injecting more combustion gas and sucking in and injecting air ahead. 【請求項２２４】 撥水性タービン翼を具備した全動翼
蒸気タービンの燃焼器兼熱交換器（４）において、燃焼
ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの
原理（９１）を利用して１以上複数の水噴射装置（９
３）より燃焼ガスを噴射し、前方の水を吸引して噴射す
ることを特徴とする全動翼蒸気ガスタービン合体機関。224. In a combustor / heat exchanger (4) of an all-blade steam turbine equipped with a water-repellent turbine blade, a combustion gas outlet (88) is provided at a combustion gas outlet, and a spraying principle (91) is provided. One or more water injection devices (9
3) A combustion engine with integrated moving blades, which injects combustion gas from 3) and sucks and injects water in front. 【請求項２２５】 撥水性タービン翼を具備した全動翼
ガスタービンの燃焼器兼熱交換器（４）において、霧吹
きの原理を利用して１以上複数の特殊装置（９２）より
過熱蒸気を噴射し、前方の空気を吸引して噴射推進し、
該出力で駆動する装置を具備したことを特徴とする全動
翼蒸気ガスタービン合体機関。225. In a combustor / heat exchanger (4) of an all moving blade gas turbine equipped with a water repellent turbine blade, superheated steam is injected from one or more special devices (92) by utilizing the principle of atomization. Then, suck the air in front and propel the jet,
An all-blade steam gas turbine integrated engine comprising a device driven by the output. 【請求項２２６】 撥水性タービン翼を具備した全動翼
ガスタービンの燃焼器兼熱交換器（４）において、霧吹
きの原理を利用して１以上複数の水噴射装置（９３）よ
り過熱蒸気を噴射し、前方の水を吸引して噴射推進し、
該出力で駆動する装置を具備したことを特徴とする全動
翼蒸気ガスタービン合体機関。226. In a combustor / heat exchanger (4) of an all-blade gas turbine equipped with water repellent turbine blades, superheated steam is generated from one or more water injection devices (93) by utilizing the principle of atomization. Inject the water, suck the water in front and propel it,
An all-blade steam gas turbine integrated engine comprising a device driven by the output. 【請求項２２７】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
霧吹きの原理（９１）を利用して１以上複数の特殊装置
（９２）より過熱蒸気を噴射し、前方の空気を吸引して
噴射推進し、該出力で駆動する装置を具備したことを特
徴とする全動翼蒸気ガスタービン合体機関。227. A combustor and heat exchanger (4) for an all-blade steam gas turbine equipped with a water-repellent turbine blade,
A device for injecting superheated steam from one or more special devices (92) utilizing the principle of atomization (91), sucking forward air to inject and propel it, and driving it with the output is provided. Combined full-blade steam gas turbine engine. 【請求項２２８】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
霧吹きの原理（９１）を利用して１以上複数の水噴射装
置（９３）より過熱蒸気を噴射し、前方の水を吸引して
噴射推進し、該出力で駆動する装置を具備したことを特
徴とする全動翼蒸気ガスタービン合体機関。228. A combustor and heat exchanger (4) for a full-blade steam gas turbine comprising a water-repellent turbine blade,
It is equipped with a device for injecting superheated steam from one or more water injection devices (93) by using the principle of atomization (91), sucking water in front of the device, propelling it, and driving it with the output. Combined full-blade steam gas turbine engine. 【請求項２２９】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹
きの原理（９１）を利用して夫々の１以上複数の特殊装
置（９２）より過熱蒸気及び燃焼ガスを噴射し、前方の
空気を吸引して噴射推進し、該出力で駆動する装置を具
備したことを特徴とする全動翼蒸気ガスタービン合体機
関。229. A combustor and heat exchanger (4) for an all-blade steam gas turbine equipped with a water-repellent turbine blade,
A combustion gas outlet (88) is provided at the combustion gas outlet, and superheated steam and combustion gas are injected from each of one or more special devices (92) by utilizing the principle of atomization (91), and the air in front is An all-blade steam gas turbine integrated engine comprising a device which is sucked, propelled and propelled, and driven by the output. 【請求項２３０】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹
きの原理（９１）を利用して夫々の１以上複数の水噴射
装置（９３）より過熱蒸気及び燃焼ガスを噴射し、前方
の水を吸引して噴射推進し、該出力で駆動する装置を具
備したことを特徴とする全動翼蒸気ガスタービン合体機
関。230. A combustor and heat exchanger (4) for an all-blade steam gas turbine equipped with a water-repellent turbine blade,
A combustion gas outlet (88) is provided at the combustion gas outlet, and superheated steam and combustion gas are injected from each of one or more water injection devices (93) by utilizing the principle of atomization (91), and water in front is discharged. An all-blade steam gas turbine integrated engine, which is equipped with a device for sucking and propelling and propelling the fuel, and driving with the output. 【請求項２３１】 撥水性タービン翼を具備した全動翼
蒸気タービンの燃焼器兼熱交換器（４）において、燃焼
ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの
原理（９１）を利用して夫々の１以上複数の特殊装置
（９２）より過熱蒸気及び燃焼ガスを噴射し、前方の空
気を吸引して噴射推進し、該出力で駆動する装置を具備
したことを特徴とする全動翼蒸気ガスタービン合体機
関。231. In a combustor / heat exchanger (4) of an all-blade steam turbine equipped with a water-repellent turbine blade, a combustion gas outlet (88) is provided at a combustion gas outlet, and a spraying principle (91) is provided. Is used to inject superheated steam and combustion gas from each of one or more special devices (92), suck front air, inject and propel it, and drive it with the output. Full rotor steam gas turbine combined engine. 【請求項２３２】 撥水性タービン翼を具備した全動翼
蒸気タービンの燃焼器兼熱交換器（４）において、燃焼
ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの
原理（９１）を利用して夫々の１以上複数の水噴射装置
（９３）より過熱蒸気及び燃焼ガスを噴射し、前方の水
を吸引して噴射推進し、該出力で駆動する装置を具備し
たことを特徴とする全動翼蒸気ガスタービン合体機関。232 In a combustor and heat exchanger (4) of an all-blade steam turbine equipped with a water repellent turbine blade, a combustion gas outlet (88) is provided at a combustion gas outlet, and a spraying principle (91) is provided. By utilizing the above to inject superheated steam and combustion gas from one or more water injecting devices (93) respectively, suck water in front and inject and propel it, and drive it with the output. Combined full-blade steam gas turbine engine. 【請求項２３３】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹
きの原理（９１）を利用して１以上複数の特殊装置（９
２）より燃焼ガスを噴射し、前方の空気を吸引して噴射
推進し、該出力で駆動する装置を具備したことを特徴と
する全動翼蒸気ガスタービン合体機関。233. A combustor and heat exchanger (4) for an all-blade steam gas turbine equipped with a water-repellent turbine blade,
A combustion gas outlet (88) is provided at the combustion gas outlet to utilize one or more special devices (9) by utilizing the atomization principle (91).
2) An all-blade steam gas turbine integrated engine equipped with a device for injecting combustion gas from 2), sucking in air in the front, injecting and propelling it, and driving it with the output. 【請求項２３４】 撥水性タービン翼を具備した全動翼
蒸気ガスタービンの燃焼器兼熱交換器（４）において、
燃焼ガス出口に燃焼ガス取出口（８８）を設けて、霧吹
きの原理（９１）を利用して１以上複数の水噴射装置
（９３）より燃焼ガスを噴射し、前方の水を吸引して噴
射推進し、該出力で駆動する装置を具備したことを特徴
とする全動翼蒸気ガスタービン合体機関。234. A combustor and heat exchanger (4) for an all-blade steam gas turbine equipped with a water-repellent turbine blade,
A combustion gas outlet (88) is provided at the combustion gas outlet, and the combustion gas is injected from one or more water injection devices (93) by utilizing the atomization principle (91), and water in front is sucked and injected. An all-blade steam gas turbine united engine equipped with a device for propelling and driving with the output. 【請求項２３５】 撥水性タービン翼を具備した全動翼
蒸気タービンの燃焼器兼熱交換器（４）において、燃焼
ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの
原理（９１）を利用して１以上複数の特殊装置（９２）
より燃焼ガスを噴射し、前方の空気を吸引して噴射推進
し、該出力で駆動する装置を具備したことを特徴とする
全動翼蒸気ガスタービン合体機関。235. In a combustor / heat exchanger (4) of an all-blade steam turbine equipped with a water-repellent turbine blade, a combustion gas outlet (88) is provided at a combustion gas outlet, and a spraying principle (91) is provided. One or more special devices using (92)
An all-blade steam gas turbine integrated engine comprising a device for injecting more combustion gas, sucking forward air for injection and propelling, and driving with the output. 【請求項２３６】 撥水性タービン翼を具備した全動翼
蒸気タービンの燃焼器兼熱交換器（４）において、燃焼
ガス出口に燃焼ガス取出口（８８）を設けて、霧吹きの
原理（９１）を利用して１以上複数の水噴射装置（９
３）より燃焼ガスを噴射し、前方の水を吸引して噴射推
進し、該出力で駆動する装置を具備したことを特徴とす
る全動翼蒸気ガスタービン合体機関。236. In a combustor / heat exchanger (4) of an all-blade steam turbine equipped with a water-repellent turbine blade, a combustion gas outlet (88) is provided at a combustion gas outlet, and a spraying principle (91) is provided. One or more water injection devices (9
3) An all-blade steam gas turbine combined engine equipped with a device for injecting combustion gas from 3), sucking in water in the front, injecting and propelling it, and driving it with the output. 【請求項２３７】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）の各種着磁摩擦車や各種磁着
摩擦車は、回転方向上流側に、電磁石（３４）を設け
て、夫々適宜に互換して使用すると共に、途中水路を水
噴射手段に連絡したことを特徴とする全動翼蒸気ガスタ
ービン合体機関。237. The various magnetic friction wheels and the various magnetic friction wheels of the magnetic friction power transmission device (14) that also serves as the friction pump (97) are respectively provided with an electromagnet (34) on the upstream side in the rotation direction. An all-blade steam gas turbine integrated engine characterized in that it is used interchangeably as appropriate and has a waterway connected to a water injection means on the way. 【請求項２３８】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）の各種着磁摩擦車や各種磁着
摩擦車は、回転方向上流側に、棒磁石（３３）を設け
て、夫々適宜に互換して使用すると共に、途中水路を水
噴射手段に連絡したことを特徴とする全動翼蒸気ガスタ
ービン合体機関。238. The various magnetic friction wheels and the various magnetic friction wheels of the magnetic friction power transmission device (14) also serving as the friction pump (97) are provided with a bar magnet (33) on the upstream side in the rotation direction, An all-blade steam gas turbine integrated engine, characterized in that they are used interchangeably as appropriate and that a waterway is connected to a water injection means on the way. 【請求項２３９】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）の各種着磁摩擦車や各種磁着
摩擦車は、回転方向下流側に、電磁石（３４）を設け
て、夫々適宜に互換して使用すると共に、途中水路を水
噴射手段に連絡したことを特徴とする全動翼蒸気ガスタ
ービン合体機関。239. The various magnetic friction wheels and the various magnetic friction wheels of the magnetic friction power transmission device (14) that also serves as the friction pump (97) are respectively provided with an electromagnet (34) on the downstream side in the rotation direction. An all-blade steam gas turbine integrated engine characterized in that it is used interchangeably as appropriate and has a waterway connected to a water injection means on the way. 【請求項２４０】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）の各種着磁摩擦車や各種磁着
摩擦車は、回転方向下流側に、棒磁石（３３）を設け
て、夫々適宜に互換して使用すると共に、途中水路を水
噴射手段に連絡したことを特徴とする全動翼蒸気ガスタ
ービン合体機関。240. The magnetized friction wheel and the magnetized friction wheel of the magnetic friction power transmission device (14) also serving as the friction pump (97) are provided with a bar magnet (33) on the downstream side in the rotation direction, An all-blade steam gas turbine integrated engine, characterized in that they are used interchangeably as appropriate and that a waterway is connected to a water injection means on the way. 【請求項２４１】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）の各種内着磁摩擦車や各種内
磁着摩擦車は、回転方向上流側及び下流側に、電磁石
（３４）を設けて、夫々適宜に互換して使用すると共
に、途中水路を水噴射手段に連絡したことを特徴とする
全動翼蒸気ガスタービン合体機関。241. The various internally magnetized friction wheels and various internally magnetized friction wheels of the magnetic friction power transmission device (14) which also serves as the friction pump (97), have electromagnets (34) on the upstream and downstream sides in the rotational direction. Is provided and used in an appropriately compatible manner, and a midway water channel is connected to a water injection means. 【請求項２４２】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）の各種内着磁摩擦車や各種内
磁着摩擦車は、回転方向上流側及び下流側に、棒磁石
（３３）を設けて、夫々適宜に互換して使用すると共
に、途中水路を水噴射手段に連絡したことを特徴とする
全動翼蒸気ガスタービン合体機関。242. The various internally magnetized friction wheels and the various internally magnetized friction wheels of the magnetic friction power transmission device (14) also serving as the friction pump (97) are provided with bar magnets (33) on the upstream and downstream sides in the rotation direction. ) Are provided and used interchangeably as appropriate, and the midway water channel is connected to the water injection means, and the all-blade steam gas turbine integrated engine is characterized. 【請求項２４３】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）の各種内着磁摩擦車や各種内
磁着摩擦車は、回転方向上流側に、電磁石（３４）を設
けて、夫々適宜に互換して使用すると共に、途中水路を
水噴射手段に連絡したことを特徴とする全動翼蒸気ガス
タービン合体機関。243. The various internally magnetized friction wheels and the various internally magnetized friction wheels of the magnetic friction power transmission device (14) also serving as the friction pump (97) have an electromagnet (34) provided on the upstream side in the rotational direction. A fully moving blade steam gas turbine combined engine, characterized in that the water channels are connected to the water injection means in the middle while being used interchangeably as appropriate. 【請求項２４４】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）の各種内着磁摩擦車や各種内
磁着摩擦車は、回転方向上流側に、棒磁石（３３）を設
けて、夫々適宜に互換して使用すると共に、途中水路を
水噴射手段に連絡したことを特徴とする全動翼蒸気ガス
タービン合体機関。244. The various internally magnetized friction wheels and various internally magnetized friction wheels of the magnetic friction power transmission device (14) which also serves as the friction pump (97) are provided with a bar magnet (33) on the upstream side in the rotational direction. In addition, the full-blade steam gas turbine integrated engine is characterized in that the water channels are connected to the water injection means on the way while being used interchangeably as appropriate. 【請求項２４５】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）の各種内着磁摩擦車や各種内
磁着摩擦車は、回転方向下流側に、電磁石（３４）を設
けて、夫々適宜に互換して使用すると共に、途中水路を
水噴射手段に連絡したことを特徴とする全動翼蒸気ガス
タービン合体機関。245. Various internally magnetized friction wheels and various internally magnetized friction wheels of the magnetic friction power transmission device (14) which also serves as the friction pump (97), have an electromagnet (34) provided on the downstream side in the rotational direction. A fully moving blade steam gas turbine combined engine, characterized in that the water channels are connected to the water injection means in the middle while being used interchangeably as appropriate. 【請求項２４６】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）の各種内着磁摩擦車や各種内
磁着摩擦車は、回転方向下流側に、棒磁石（３３）を設
けて、夫々適宜に互換して使用すると共に、途中水路を
水噴射手段に連絡したことを特徴とする全動翼蒸気ガス
タービン合体機関。246. The various internally magnetized friction wheels and various internally magnetized friction wheels of the magnetic friction power transmission device (14) which also serves as the friction pump (97) are provided with a bar magnet (33) on the downstream side in the rotational direction. In addition, the full-blade steam gas turbine integrated engine is characterized in that the water channels are connected to the water injection means on the way while being used interchangeably as appropriate. 【請求項２４７】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）により、燃焼器兼熱交換器
（４）に供給する水を昇圧して使用すると共に、途中水
路を水噴射手段に連絡したことを特徴とする全動翼蒸気
ガスタービン合体機関。247. The magnetic friction power transmission device (14) which also functions as the friction pump (97) boosts the pressure of the water supplied to the combustor and heat exchanger (4) for use, and the water channel in the middle of the water injection means. Full-blade steam gas turbine coalescence engine characterized by contacting. 【請求項２４８】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）により、燃焼器兼熱交換器
（４）に供給する水を多段に昇圧して使用すると共に、
途中水路を水噴射手段に連絡したことを特徴とする全動
翼蒸気ガスタービン合体機関。248. The magnetic friction power transmission device (14) which also functions as the friction pump (97) multiplies the water supplied to the combustor and heat exchanger (4) for use, and
An all-blade steam gas turbine integrated engine characterized in that a waterway is connected to a water injection means on the way. 【請求項２４９】 前記複数の摩擦ポンプ（９７）兼用
の磁気摩擦動力伝達装置（１４）により、燃焼器兼熱交
換器（４）に供給する水を多段に昇圧して使用すると共
に、途中水路を水噴射手段に連絡したことを特徴とする
全動翼蒸気ガスタービン合体機関。249. The magnetic friction power transmission device (14) also serving as the plurality of friction pumps (97) is used to increase the pressure of the water supplied to the combustor and heat exchanger (4) in multiple stages and to use the intermediate water passage. An all-blade steam gas turbine integrated engine, characterized in that the water is connected to a water injection means. 【請求項２５０】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）は、燃焼器兼熱交換器（４）
に供給する水を使用すると共に、途中水路を水噴射手段
に連絡したことを特徴とする全動翼蒸気ガスタービン合
体機関。250. A magnetic friction power transmission device (14) also serving as the friction pump (97), comprising a combustor and heat exchanger (4).
An all-blade steam gas turbine integrated engine characterized by using water to be supplied to a water injection means and connecting a waterway on the way to a water injection means. 【請求項２５１】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）は、燃焼器兼熱交換器（４）
に供給する水を使用すると共に、該水圧上昇により摩擦
ポンプ（９７）を非接触に近付けると共に、途中水路を
水噴射手段に連絡したことを特徴とする全動翼蒸気ガス
タービン合体機関。251. A magnetic friction power transmission device (14) also serving as the friction pump (97), comprising a combustor and heat exchanger (4).
A full-blade steam-gas turbine integrated engine, characterized in that the water supplied to the pump is used, the friction pump (97) is brought into non-contact with the water pressure increase, and the water channel is connected to the water injection means on the way. 【請求項２５２】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）は、燃焼器兼熱交換器（４）
に供給する水を使用すると共に、該水圧上昇により摩擦
ポンプ（９７）を非接触に近付けて超高速回転に対応す
ると共に、途中水路を水噴射手段に連絡したことを特徴
とする全動翼蒸気ガスタービン合体機関。252. A magnetic friction power transmission device (14) also serving as the friction pump (97) comprises a combustor and heat exchanger (4).
And the water is supplied to the friction pump (97) so as to bring the friction pump (97) close to a non-contact state to cope with ultra-high speed rotation by the water pressure increase, and a midway water channel is connected to the water injection means. Gas turbine united engine. 【請求項２５３】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）は、燃焼器兼熱交換器（４）
に供給する水を使用すると共に、該水温を上昇して使用
すると共に、途中水路を水噴射手段に連絡したことを特
徴とする全動翼蒸気ガスタービン合体機関。253. A magnetic friction power transmission device (14) also serving as the friction pump (97) comprises a combustor and heat exchanger (4).
An all-blade steam gas turbine integrated engine, characterized in that the water supplied to the water is used, the water temperature is raised and used, and a water channel is connected to the water injection means on the way. 【請求項２５４】 前記摩擦ポンプ（９７）兼用の磁気
摩擦動力伝達装置（１４）は、燃焼器兼熱交換器（４）
に供給する水を使用すると共に水温を上昇して使用し、
該水に物質を混入して公害低減し、潤滑すると共に、途
中水路を水噴射手段に連絡したことを特徴とする全動翼
蒸気ガスタービン合体機関。254. A magnetic friction power transmission device (14) also serving as the friction pump (97) comprises a combustor and heat exchanger (4).
Use the water supplied to and raise the water temperature,
A full-blade steam gas turbine integrated engine characterized in that a substance is mixed into the water to reduce pollution and lubricate, and a waterway is connected to a water injection means on the way. 【請求項２５５】 前記水噴射手段（５６）は組立環状
接続部付近に設け、翼段落毎に環状に一体鋳造（８４）
して、該組立環状接続部で水路を接続使用することを特
徴とする撥水性タービン翼を具備した全動翼蒸気ガスタ
ービン合体機関。255. The water injection means (56) is provided in the vicinity of an assembled annular connecting portion, and is integrally cast in an annular shape for each blade stage (84).
Then, a full-blade steam gas turbine integrated engine equipped with a water repellent turbine blade, characterized in that a water channel is connected and used at the assembled annular connecting portion. 【請求項２５６】 前記水噴射手段（５６）は組立環状
接続部付近に設け、翼段落毎に環状に一体鋳造（８４）
して、該組立環状接続部で水路を接続使用し、該組立環
状接続部付近から水噴射することを特徴とする撥水性タ
ービン翼を具備した全動翼蒸気ガスタービン合体機関。256. The water injection means (56) is provided in the vicinity of an assembled annular connecting portion, and is integrally cast in an annular shape for each blade stage (84).
Then, a water turbine is connected at the assembled annular connecting portion, and water is injected from the vicinity of the assembled annular connecting portion to provide a water repellent turbine blade. 【請求項２５７】 前記水噴射手段（５６）は組立環状
接続部付近に設け、翼段落毎に環状に一体鋳造（８４）
して、該組立環状接続部で水路を接続使用し、該組立環
状接続部付近から水噴射して圧縮空気を冷却し、熱回収
することを特徴とする撥水性タービン翼を具備した全動
翼蒸気ガスタービン合体機関。257. The water injection means (56) is provided in the vicinity of an assembled annular connecting portion, and is integrally cast in an annular shape for each blade stage (84).
Then, a water passage is connected and used at the assembled annular connecting portion, and water is jetted from the vicinity of the assembled annular connecting portion to cool the compressed air and recover heat, so that a total blade having a water repellent turbine blade is provided. Steam gas turbine integrated engine. 【請求項２５８】 前記水噴射手段（５６）は組立環状
接続部付近に設け、翼段落毎に環状に一体鋳造（８４）
して、該組立環状接続部で水路を接続使用し、該組立環
状接続部付近から水噴射して圧縮空気を冷却し、熱回収
した冷空気を略直線蛇行的に圧縮することを特徴とする
撥水性タービン翼を具備した全動翼蒸気ガスタービン合
体機関。258. The water injection means (56) is provided in the vicinity of an assembled annular connection portion, and is integrally cast annularly for each blade stage (84).
Then, a water channel is connected and used at the assembled annular connecting portion, the compressed air is cooled by injecting water from the vicinity of the assembled annular connecting portion, and the cold air that has recovered heat is compressed in a substantially linear meandering manner. Full-blade steam gas turbine combined engine equipped with water-repellent turbine blades. 【請求項２５９】 前記水噴射手段（５６ａ）より水噴
射過熱蒸気を冷却して、過熱蒸気速度を水質量の速度エ
ネルギに変換することを特徴とする撥水性タービン翼を
具備した全動翼蒸気ガスタービン合体機関。259. A total moving blade steam equipped with a water repellent turbine blade, characterized in that the water injection superheated steam is cooled by said water injection means (56a) to convert the superheated steam velocity into velocity energy of water mass. Gas turbine united engine. 【請求項２６０】 前記水噴射手段（５６ａ）より水噴
射過熱蒸気を冷却して、過熱蒸気速度及び気化潜熱を水
質量の速度エネルギに変換することを特徴とする撥水性
タービン翼を具備した全動翼蒸気ガスタービン合体機
関。260. A water-repellent turbine blade equipped with a water-repellent turbine blade, characterized in that the water-injection superheated steam is cooled by the water injection means (56a) to convert the superheated steam velocity and latent heat of vaporization into velocity energy of water mass. Moving blade steam gas turbine combined engine. 【請求項２６１】 前記水噴射手段（５６ａ）より水噴
射過熱蒸気を冷却して、過熱蒸気速度及び気化潜熱を水
質量の速度エネルギに変換することを特徴とする撥水性
タービン翼を具備した全動翼蒸気ガスタービン合体機
関。261. A water-repellent turbine blade having a water-repellent turbine blade characterized by cooling water-jet superheated steam from said water injection means (56a) to convert superheated steam velocity and latent heat of vaporization into velocity energy of water mass. Moving blade steam gas turbine combined engine. 【請求項２６２】 前記水噴射手段（５６ａ）より水噴
射過熱蒸気を冷却して、過熱蒸気速度及び気化潜熱の大
部分を水質量の速度エネルギに変換することを特徴とす
る撥水性タービン翼を具備した全動翼蒸気ガスタービン
合体機関。262. A water repellent turbine blade, characterized in that the water injection superheated steam is cooled by the water injection means (56a) to convert most of the superheated steam velocity and latent heat of vaporization into velocity energy of water mass. Full-blade steam gas turbine integrated engine equipped. 【請求項２６３】 前記水噴射手段（５６ａ）より、水
噴射過熱蒸気を冷却して、過熱蒸気速度を水質量の速度
エネルギに変換して略直線蛇行的に噴射して出力を発生
することを特徴とする撥水性タービン翼を具備した全動
翼蒸気ガスタービン合体機関。263. The water injection means (56a) cools the water injection superheated steam, converts the superheated steam velocity into velocity energy of water mass, and injects it in a substantially linear meandering manner to generate an output. An all moving blade steam gas turbine integrated engine equipped with a characteristic water repellent turbine blade. 【請求項２６４】 前記水噴射手段（５６ａ）より、水
噴射過熱蒸気を冷却して、過熱蒸気速度及び気化潜熱を
水質量の速度エネルギに変換して、略直線蛇行的に噴射
して出力を発生することを特徴とする撥水性タービン翼
を具備した全動翼蒸気ガスタービン合体機関。264. The water injection means (56a) cools the water injection superheated steam, converts the superheated steam velocity and latent heat of vaporization into velocity energy of water mass, and injects in a substantially straight line meandering manner to output. An all-blade steam gas turbine integrated engine equipped with a water-repellent turbine blade characterized by being generated. 【請求項２６５】 前記水噴射手段（５６ａ）より、水
噴射過熱蒸気を冷却して、過熱蒸気速度及び気化潜熱を
水質量の速度エネルギに変換して、略直線蛇行的に噴射
して出力を発生することを特徴とする撥水性タービン翼
を具備した全動翼蒸気ガスタービン合体機関。265. The water injection means (56a) cools the water injection superheated steam, converts the superheated steam velocity and latent heat of vaporization into velocity energy of water mass, and injects it in a substantially straight line meandering manner to output. An all-blade steam gas turbine integrated engine equipped with a water-repellent turbine blade characterized by being generated. 【請求項２６６】 前記水噴射手段（５６ａ）より、水
噴射過熱蒸気を冷却して、過熱蒸気速度及び気化潜熱の
大部分を水質量の速度エネルギに変換して略直線蛇行的
に噴射して出力を発生することを特徴とする撥水性ター
ビン翼を具備した全動翼蒸気ガスタービン合体機関。266. The water injection means (56a) cools the water injection superheated steam, converts most of the superheated steam velocity and latent heat of vaporization into velocity energy of water mass, and injects it in a substantially linear meandering manner. An all- moving blade steam gas turbine integrated engine equipped with a water-repellent turbine blade, which is characterized by generating output. 【請求項２６７】 前記水噴射手段（５６ａ）は組立環
状接続部付近に設け、翼段落毎に環状に一体鋳造（８
４）して、該組立環状接続部で断熱した水路を接続使用
することを特徴とする撥水性タービン翼を具備した全動
翼蒸気ガスタービン合体機関。267. The water injection means (56a) is provided in the vicinity of an assembled annular connecting portion, and is integrally cast in an annular shape for each blade stage (8).
4) Then, an all-blade steam gas turbine integrated engine equipped with a water-repellent turbine blade, characterized in that a water passage insulated by the assembled annular connection portion is used for connection. 【請求項２６８】 前記水噴射手段（５６ａ）は、翼段
落毎に環状に一体鋳造（８４）した外側タービン動翼群
（１９）及び内側タービン動翼群（２０）の、いずれか
の組立環状接続部付近に設けたことを特徴とする撥水性
タービン翼を具備した全動翼蒸気ガスタービン合体機
関。268. The water injection means (56a) is an assembled annular shape of an outer turbine rotor blade group (19) and an inner turbine rotor blade group (20) which are integrally cast (84) annularly for each blade stage. A full-blade steam gas turbine integrated engine equipped with a water-repellent turbine blade, characterized by being provided in the vicinity of a connecting portion. 【請求項２６９】 前記水噴射手段（５６ａ）は組立環
状接続部付近に設け、翼段落毎に環状に一体鋳造（８
４）して、該組立環状接続部で断熱した水路を接続使用
し、該組立環状接続部付近から水噴射することを特徴と
する撥水性タービン翼を具備した全動翼蒸気ガスタービ
ン合体機関。269. The water injection means (56a) is provided in the vicinity of an assembled annular connecting portion, and is integrally cast in an annular shape for each blade stage (8).
4) Then, a fully moving steam gas turbine integrated engine equipped with a water repellent turbine blade, characterized in that a water path insulated by the assembled annular connecting portion is connected and used, and water is injected from the vicinity of the assembled annular connecting portion. 【請求項２７０】 前記水噴射手段（５６ａ）は組立環
状接続部付近に設け、翼段落毎に環状に一体鋳造（８
４）して、該組立環状接続部で断熱した水路を接続使用
し、該組立環状接続部付近の水噴射手段（５６ａ）から
水噴射して、燃焼ガス容積を縮小して質量を増大するこ
とを特徴とする撥水性タービン翼を具備した全動翼蒸気
ガスタービン合体機関。270. The water injection means (56a) is provided in the vicinity of an assembled annular connecting portion, and is integrally cast in an annular shape for each blade stage (8).
4) Then, by connecting and using a water channel insulated by the assembled annular connection portion, water is injected from the water injection means (56a) near the assembled annular connection portion to reduce the combustion gas volume and increase the mass. An all-blade steam-gas turbine combined engine equipped with a water-repellent turbine blade. 【請求項２７１】 前記水噴射手段（５６ａ）は組立環
状接続部付近に設け、翼段落毎に環状に一体鋳造（８
４）して、該組立環状接続部で断熱した水路を接続使用
し、該組立環状接続部付近の水噴射手段（５６ａ）から
水噴射して、過熱蒸気容積を縮小して質量を増大するこ
とを特徴とする撥水性タービン翼を具備した全動翼蒸気
ガスタービン合体機関。271. The water injection means (56a) is provided in the vicinity of an assembled annular connection portion, and is integrally cast in an annular shape for each blade stage (8).
4) Then, by connecting and using a water path insulated by the assembled annular connection portion, water is injected from the water injection means (56a) near the assembled annular connection portion to reduce the superheated steam volume and increase the mass. An all-blade steam-gas turbine combined engine equipped with a water-repellent turbine blade. 【請求項２７２】 前記水噴射手段（５６ａ）は組立環
状接続部付近に設け、翼段落毎に環状に一体鋳造（８
４）して、該組立環状接続部で断熱した水路を接続して
使用し、該組立環状接続部付近の水噴射手段（５６ａ）
から水噴射し、該水に有害物質を合成溶解を促進する物
質を含めたことを特徴とする撥水性タービン翼を具備し
た全動翼蒸気ガスタービン合体機関。272. The water injection means (56a) is provided in the vicinity of the assembled annular connecting portion, and is integrally cast in an annular shape for each blade stage (8).
4) Then, the water passage insulated by the assembled annular connecting portion is connected and used, and water injection means (56a) near the assembled annular connecting portion is used.
A steam turbine integrated turbine engine equipped with a water repellent turbine blade, characterized in that a water-injected water is included in the water, and a substance that promotes synthetic dissolution of a harmful substance is included in the water. 【請求項２７３】 前記水噴射手段（５６ａ）は組立環
状接続部付近に設け、翼段落毎に環状に一体鋳造（８
４）して、該組立環状接続部で断熱した水路を接続して
使用し、該組立環状接続部付近から水噴射し、該水に有
害物質を合成溶解を促進する物質を含めて、無害に近付
けて排出することを特徴とする撥水性タービン翼を具備
した全動翼蒸気ガスタービン合体機関。273. The water injection means (56a) is provided in the vicinity of an assembled annular connecting portion, and is integrally cast in an annular shape for each blade stage (8).
4) Then, a water channel insulated by the assembled annular connecting portion is connected and used, and water is injected from the vicinity of the assembled annular connecting portion to harmlessly include a substance that promotes synthetic dissolution of harmful substances in the water. An all-blade steam-gas turbine integrated engine equipped with a water-repellent turbine blade, which is characterized in that it is discharged in close proximity. 【請求項２７４】 前記水により撥水性水冷却翼（８
７）を冷却後に、組立環状接続部付近に設けた水噴射手
段（５６）より水噴射する組立環状接続部は、翼段落毎
に環状に一体鋳造（８４）して、該組立環状接続部で冷
却手段（５５）の水路を接続使用することを特徴とする
撥水性タービン翼を具備した全動翼蒸気ガスタービン合
体機関。274. A water-repellent water cooling blade (8)
After cooling 7), the assembled annular connecting portion for injecting water from the water injecting means (56) provided near the assembled annular connecting portion is integrally cast (84) in an annular shape for each blade stage, and the assembled annular connecting portion An all-blade steam gas turbine integrated engine equipped with a water-repellent turbine blade, characterized in that a water passage of a cooling means (55) is connected and used. 【請求項２７５】 前記水により撥水性水冷却翼を冷却
後に水噴射手段（５６）より水噴射する組立環状接続部
は、翼段落毎に環状に一体鋳造（８４）して、該組立環
状接続部で冷却手段（５５）の水路を接続使用すること
を特徴とする撥水性タービン翼を具備した全動翼蒸気ガ
スタービン合体機関。275. An assembled annular connection portion for injecting water from a water injection means (56) after cooling the water-repellent water cooling blade with the water is integrally cast (84) in an annular shape for each blade stage, and the assembled annular connection is formed. An all-blade steam gas turbine combined engine equipped with a water-repellent turbine blade, characterized in that a water passage of a cooling means (55) is connected and used in a part. 【請求項２７６】 前記水により１以上複数の撥水性水
冷却翼を冷却後に水噴射手段（５６）より水噴射する組
立環状接続部は、翼段落毎に環状に一体鋳造（８４）し
て、該組立環状接続部で冷却手段（５５）の水路を接続
使用することを特徴とする撥水性タービン翼を具備した
全動翼蒸気ガスタービン合体機関。276. An assembled annular connecting portion for injecting water from a water injecting means (56) after cooling one or more water repellent water cooling blades with the water is integrally cast (84) in an annular shape for each blade stage, A full-blade steam gas turbine integrated engine equipped with a water-repellent turbine blade, characterized in that a water passage of a cooling means (55) is connected and used at the assembled annular connection portion. 【請求項２７７】 前記水により段落全部の撥水性水冷
却翼を冷却後に水噴射手段（５６）より水噴射する組立
環状接続部は、翼段落毎に環状に一体鋳造（８４）し
て、該組立環状接続部で冷却手段（５５）の水路を接続
使用することを特徴とする撥水性タービン翼を具備した
全動翼蒸気ガスタービン合体機関。277. An assembled annular connecting portion for injecting water from the water injecting means (56) after cooling all the water repellent water cooling blades with the water is integrally cast (84) in an annular shape for each blade paragraph, An all-blade steam-gas turbine integrated engine equipped with a water-repellent turbine blade, characterized in that a water passage of a cooling means (55) is connected and used at an assembled annular connection portion. 【請求項２７８】 前記水により段落半分の撥水性水冷
却翼を冷却後に水噴射手段（５６）より水噴射する組立
環状接続部は、翼段落毎に環状に一体鋳造（８４）し
て、該組立環状接続部で冷却手段（５５）の水路を接続
使用することを特徴とする撥水性タービン翼を具備した
全動翼蒸気ガスタービン合体機関。278. The assembled annular connecting portion for injecting water from the water injecting means (56) after cooling the water repellent water cooling blade of the half of the paragraph with the water is integrally cast (84) in an annular shape for each blade paragraph, An all-blade steam-gas turbine integrated engine equipped with a water-repellent turbine blade, characterized in that a water passage of a cooling means (55) is connected and used at an assembled annular connection portion. 【請求項２７９】 前記燃焼ガス排気温度を−２７３℃
に近付けることで、全動翼蒸気ガスタービンの熱回収量
を増大することを特徴とする撥水性タービン翼を具備し
た全動翼蒸気ガスタービン合体機関。279. The combustion gas exhaust gas temperature is -273 ° C.
A full-blade steam gas turbine integrated engine equipped with a water-repellent turbine blade, characterized in that the amount of heat recovery of the full-blade steam gas turbine is increased by approaching 【請求項２８０】 前記燃焼ガス排気温度を−２７３℃
に近付けることで、全動翼ガスタービンの熱回収量を増
大することを特徴とする撥水性タービン翼を具備した全
動翼蒸気ガスタービン合体機関。280. The combustion gas exhaust gas temperature is -273 ° C.
A full-blade steam gas turbine combined engine equipped with a water-repellent turbine blade, which is characterized by increasing the amount of heat recovery of the full-blade gas turbine. 【請求項２８１】 前記燃焼ガス排気温度を−２７３℃
に近付けることで、全動翼蒸気ガスタービンの排気近傍
で、極低温燃焼ガスを核に凝集する水蒸気等の凝集を容
易にすることを特徴とする撥水性タービン翼を具備した
全動翼蒸気ガスタービン合体機関。281. The combustion gas exhaust gas temperature is -273 ° C.
Near the exhaust gas of the full-blade steam gas turbine, facilitating the agglomeration of water vapor etc. that agglomerate the cryogenic combustion gas into the core, a full-blade steam gas equipped with a water-repellent turbine blade Turbine united engine. 【請求項２８２】 前記燃焼ガス排気温度を−２７３℃
に近付けることで、全動翼ガスタービンの排気近傍で、
極低温燃焼ガスを核に凝集する水蒸気等の凝集を容易に
することを特徴とする撥水性タービン翼を具備した全動
翼蒸気ガスタービン合体機関。282. The combustion gas exhaust temperature is -273 ° C.
Near the exhaust gas of the rotor blade gas turbine,
A full-blade steam-gas turbine integrated engine equipped with a water-repellent turbine blade, which facilitates the agglomeration of steam or the like that agglomerates a cryogenic combustion gas into a nucleus. 【請求項２８３】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収して、海中に供給することを特徴
とする撥水性タービン翼を具備した全動翼蒸気ガスター
ビン合体機関。283. The combustion gas exhaust temperature is set to −273 ° C.
A water repellent turbine characterized by aggregating water and steam with cryogenic combustion gas as a core in a combined engine of all moving blade steam gas turbines, which is separated and collected as hail and water droplets and supplied into the sea. Full-blade steam gas turbine integrated engine equipped with blades. 【請求項２８４】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収し、海中に供給して、海藻類を繁
殖させることを特徴とする撥水性タービン翼を具備した
全動翼蒸気ガスタービン合体機関。284. The combustion gas exhaust temperature is set to -273 ° C.
In an all-blade steam gas turbine coalescence engine, which is closer to, agglomerates water and steam with a cryogenic combustion gas as a nucleus, separates and collects them as hail and water droplets, and supplies them to the sea to propagate seaweeds. An all moving blade steam gas turbine integrated engine equipped with a characteristic water repellent turbine blade. 【請求項２８５】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収し、海中に供給して、珊瑚類を繁
殖させることを特徴とする撥水性タービン翼を具備した
全動翼蒸気ガスタービン合体機関。285. The combustion gas exhaust temperature is set to −273 ° C.
In an all-blade steam gas turbine coalescence engine, which is closer to the An all moving blade steam gas turbine integrated engine equipped with a characteristic water repellent turbine blade. 【請求項２８６】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収し、海中に供給して、魚介類を繁
殖させることを特徴とする撥水性タービン翼を具備した
全動翼蒸気ガスタービン合体機関。286. The combustion gas exhaust gas temperature is -273 ° C.
In an all-blade steam gas turbine coalescence engine, which is closer to, agglomerates water and steam with a cryogenic combustion gas as a nucleus, separates and collects them as hail and water droplets, and supplies them to the sea to breed seafood. An all moving blade steam gas turbine integrated engine equipped with a characteristic water repellent turbine blade. 【請求項２８７】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収して、海水を冷却する過程で酸素
等を吸入して、海中に供給することを特徴とする撥水性
タービン翼を具備した全動翼蒸気ガスタービン合体機
関。287. The combustion gas exhaust gas temperature is set to −273 ° C.
In an all-blade steam gas turbine coalescence engine, which is closer to, aggregates water and steam with cryogenic combustion gas as a core, separates and collects as hail, water droplets, etc., and inhales oxygen etc. in the process of cooling seawater. , A full-blade steam gas turbine integrated engine equipped with a water-repellent turbine blade, which is supplied to the sea. 【請求項２８８】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収して、酸素等と共に海中に供給し
て、海藻類を繁殖させることを特徴とする撥水性タービ
ン翼を具備した全動翼蒸気ガスタービン合体機関。288. The combustion gas exhaust gas temperature is -273 ° C.
In an all-blade steam gas turbine coalescence engine, which is closer to, aggregates water and water vapor with cryogenic combustion gas as a nucleus, separates and collects it as hail, water droplets, etc., and supplies it to the sea with oxygen etc. An all-blade steam gas turbine integrated engine equipped with a water-repellent turbine blade characterized by being propagated. 【請求項２８９】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収して、酸素等と共に海中に供給し
て、珊瑚類を繁殖させることを特徴とする撥水性タービ
ン翼を具備した全動翼蒸気ガスタービン合体機関。289. The combustion gas exhaust gas temperature is set to −273 ° C.
In an all-blade steam gas turbine coalescing engine, which is closer to, aggregates water and water vapor with a cryogenic combustion gas as a nucleus, separates and collects it as hail, water droplets, etc., and supplies it to the sea together with oxygen, etc. An all-blade steam gas turbine integrated engine equipped with a water-repellent turbine blade characterized by being propagated. 【請求項２９０】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収して、酸素等と共に海中に供給し
て、微生物や魚介類を繁殖させることを特徴とする撥水
性タービン翼を具備した全動翼蒸気ガスタービン合体機
関。290. The combustion gas exhaust gas temperature is -273 ° C.
In an all-blade steam-gas turbine coalescence engine, which is closer to the water, a cryogenic combustion gas is used as a core to coagulate water and water vapor, which is separated and collected as hail, water droplets, etc., and supplied to the sea along with oxygen, etc. An all-blade steam-gas turbine united engine equipped with a water-repellent turbine blade, which is characterized in that it breeds species. 【請求項２９１】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収して、水道水を冷却することを特
徴とする撥水性タービン翼を具備した全動翼蒸気ガスタ
ービン合体機関。291. The combustion gas exhaust gas temperature is -273 ° C.
In a combined engine with all moving blades of a steam gas turbine, water and water vapor are condensed by using cryogenic combustion gas as a nucleus, separated and collected as hail and water droplets, and the tap water is cooled. A fully moving steam gas turbine combined engine equipped with turbine blades. 【請求項２９２】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収して、水道水を冷却して冷熱で貯
蔵することを特徴とする撥水性タービン翼を具備した全
動翼蒸気ガスタービン合体機関。292. The combustion gas exhaust gas temperature is set to −273 ° C.
In an all-blade steam-gas turbine combined engine, which is closer to the above, the cryogenic combustion gas is used as a core to coagulate water and water vapor, and is separated and collected as hail, water droplets, etc., and the tap water is cooled and stored in cold heat. An all moving blade steam gas turbine integrated engine equipped with a characteristic water repellent turbine blade. 【請求項２９３】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収して、水道水を冷却して冷熱で貯
蔵し、供給することを特徴とする撥水性タービン翼を具
備した全動翼蒸気ガスタービン合体機関。293. The combustion gas exhaust gas temperature is -273 ° C.
In an all-blade steam gas turbine coalescence engine, which is closer to, aggregates water and steam with cryogenic combustion gas as a core, separates and collects as hail, water droplets, etc., cools tap water, stores it in cold heat, and supplies it. An all-blade steam gas turbine united engine equipped with a water-repellent turbine blade. 【請求項２９４】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼蒸気ガスタービン合体機関におい
て、極低温燃焼ガスを核に水や水蒸気を凝集して、雹や
水滴等として分別回収して、水道水を冷却して冷熱で貯
蔵し、業務用家庭用として供給することを特徴とする撥
水性タービン翼を具備した全動翼蒸気ガスタービン合体
機関。294. The combustion gas exhaust temperature is -273 ° C.
In an all-blade steam gas turbine integrated engine, which is closer to, agglomerates water and steam with a cryogenic combustion gas as a nucleus, separates and collects it as hail, water droplets, etc., cools tap water, and stores it in cold heat. An all-blade steam gas turbine integrated engine equipped with a water-repellent turbine blade, which is supplied for domestic use. 【請求項２９５】 前記燃焼ガス排気温度を−２７３℃
に近付ける、全動翼ガスタービンにおいて、燃料の燃焼
ガス熱量の使用を略０にすることを特徴とする撥水性タ
ービン翼を具備した全動翼蒸気ガスタービン合体機関。295. The combustion gas exhaust gas temperature is -273 ° C.
In a full-rotor blade gas turbine, the use of the combustion gas heat quantity of the fuel is set to substantially zero. 【請求項２９６】 前記極低温燃焼ガスに石炭灰等を含
めて、出力発生の過程で全重力パワーを増大し、出力を
増大することを特徴とする撥水性タービン翼を具備した
全動翼蒸気ガスタービン合体機関。296. A full rotor blade steam equipped with a water repellent turbine blade, characterized in that the cryogenic combustion gas contains coal ash or the like to increase the total gravity power and increase the output in the process of generating the output. Gas turbine united engine. 【請求項２９７】 前記全動翼ガスタービン及び全動翼
蒸気タービン及び全動翼蒸気ガスタービンの、何れか１
以上の出力で駆動する装置を、大中小各種発電設備とし
たことを特徴とする全動翼蒸気ガスタービン合体機関。297. Any one of the full-blade gas turbine, the full-blade steam turbine, and the full-blade steam gas turbine.
An all-blade steam gas turbine integrated engine, characterized in that various large, medium and small power generation facilities are used as devices driven by the above outputs. 【請求項２９８】 前記全動翼ガスタービン及び全動翼
蒸気タービン及び全動翼蒸気ガスタービンの、何れか１
以上の出力で駆動する装置を、大中小各種熱と電気と冷
熱の供給設備としたことを特徴とする全動翼蒸気ガスタ
ービン合体機関。298. Any one of the full-blade gas turbine, the full-blade steam turbine, and the full-blade steam gas turbine.
An all-blade steam gas turbine integrated engine, characterized in that the device driven by the above output is a facility for supplying heat, electricity, and cold heat of various sizes. 【請求項２９９】 前記全動翼ガスタービン及び全動翼
蒸気タービン及び全動翼蒸気ガスタービンの何れか１以
上の出力で駆動する装置を、大中小各種熱と電気の供給
設備としたことを特徴とする全動翼蒸気ガスタービン合
体機関。299. A device for driving at least one of the full-blade gas turbine, the full-blade steam turbine, and the full-blade steam gas turbine is a large-medium-small heat and electricity supply facility. A featured all-blade steam gas turbine integrated engine. 【請求項３００】 前記全動翼ガスタービン及び全動翼
蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置
及び水噴射装置の何れか１以上の出力で駆動する装置
を、大中小各種船舶としたことを特徴とする全動翼蒸気
ガスタービン合体機関。300. The apparatus driven by any one or more outputs of the full-blade gas turbine, the full-blade steam turbine, the full-blade steam gas turbine, the special apparatus, and the water injection apparatus is a large, medium, or small ship. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項３０１】 前記全動翼ガスタービン及び全動翼
蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置
及び水噴射装置の何れか１以上の出力で駆動する装置
を、大中小各種航空機としたことを特徴とする全動翼蒸
気ガスタービン合体機関。301. The device driven by any one or more outputs of the full-blade gas turbine, the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device is a large, medium, or small aircraft. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項３０２】 前記全動翼ガスタービン及び全動翼
蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置
及び水噴射装置の何れか１以上の出力で駆動する装置
を、大中小各種車両としたことを特徴とする全動翼蒸気
ガスタービン合体機関。302. The apparatus driven by any one or more outputs of the full-blade gas turbine, the full-blade steam turbine, the full-blade steam gas turbine, the special apparatus, and the water injection apparatus is set to be a large, medium or small vehicle. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項３０３】 前記全動翼ガスタービン及び全動翼
蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置
及び水噴射装置の何れか１以上の出力で駆動する装置
を、大中小各種機械としたことを特徴とする全動翼蒸気
ガスタービン合体機関。303. The device driven by any one or more outputs of the full-blade gas turbine, the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device is a large, medium, or small machine. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項３０４】 前記全動翼ガスタービン及び全動翼
蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置
及び水噴射装置の何れか１以上の出力で駆動する装置
を、大中小各種艦船としたことを特徴とする全動翼蒸気
ガスタービン合体機関。304. The device driven by any one or more outputs of the full-blade gas turbine, the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device is set to various types of large, medium, and small ships. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項３０５】 前記全動翼ガスタービン及び全動翼
蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置
及び水噴射装置の何れか１以上の出力で駆動する装置
を、大中小各種戦車としたことを特徴とする全動翼蒸気
ガスタービン合体機関。305. A large, medium, or small tank is used as a device driven by any one or more outputs of the full-blade gas turbine, the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項３０６】 前記全動翼ガスタービン及び全動翼
蒸気タービン及び全動翼蒸気ガスタービン及び特殊装置
及び水噴射装置の何れか１以上の出力で駆動する装置
を、大中小各種戦闘機としたことを特徴とする全動翼蒸
気ガスタービン合体機関。306. A device for driving at least one of the full-blade gas turbine, the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device is used as a large, medium or small fighter. An all-blade steam gas turbine integrated engine characterized by the above. 【請求項３０７】 前記全動翼蒸気タービン及び全動翼
蒸気ガスタービン及び特殊装置及び水噴射装置の何れか
１以上の出力で駆動する装置を、大中小各種発電設備と
したことを特徴とする全動翼蒸気ガスタービン合体機
関。307. A device for driving with a power output of at least one of the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device is a large, medium, or small-sized power generation facility. Full rotor steam gas turbine combined engine. 【請求項３０８】 前記全動翼蒸気タービン及び全動翼
蒸気ガスタービンの何れか１以上の出力で駆動する装置
を、大中小各種熱と電気と冷熱の供給設備としたことを
特徴とする全動翼蒸気ガスタービン合体機関。308. A device driven by an output of at least one of the full-blade steam turbine and the full-blade steam gas turbine is a large-medium-small heat, electricity, and cold heat supply facility. Moving blade steam gas turbine combined engine. 【請求項３０９】 前記全動翼蒸気タービン及び全動翼
蒸気ガスタービンの何れか１以上の出力で駆動する装置
を、大中小各種熱と電気の供給設備としたことを特徴と
する全動翼蒸気ガスタービン合体機関。309. A full-rotor blade, wherein the device driven by the output of at least one of the full-rotor blade steam turbine and the full-rotor blade steam gas turbine is a facility for supplying heat and electricity of large, medium and small sizes. Steam gas turbine integrated engine. 【請求項３１０】 前記全動翼蒸気タービン及び全動翼
蒸気ガスタービン及び特殊装置及び水噴射装置の何れか
１以上の出力で駆動する装置を、大中小各種船舶とした
ことを特徴とする全動翼蒸気ガスタービン合体機関。310. A large, medium or small ship is used as the device driven by any one or more outputs of the full-blade steam turbine, the full-blade steam gas turbine, the special device and the water injection device. Moving blade steam gas turbine combined engine. 【請求項３１１】 前記全動翼蒸気タービン及び全動翼
蒸気ガスタービン及び特殊装置及び水噴射装置の何れか
１以上の出力で駆動する装置を、大中小各種航空機とし
たことを特徴とする全動翼蒸気ガスタービン合体機関。311. A large, medium or small aircraft is used as the device driven by any one or more outputs of the full-blade steam turbine, the full-blade steam gas turbine, the special device and the water injection device. Moving blade steam gas turbine combined engine. 【請求項３１２】 前記全動翼蒸気タービン及び全動翼
蒸気ガスタービン及び特殊装置及び水噴射装置の何れか
１以上の出力で駆動する装置を、大中小各種車両とした
ことを特徴とする全動翼蒸気ガスタービン合体機関。312. The apparatus driven by any one or more of the full-blade steam turbine, the full-blade steam gas turbine, the special apparatus, and the water injection apparatus is a large, medium, or small vehicle. Moving blade steam gas turbine combined engine. 【請求項３１３】 前記全動翼蒸気タービン及び全動翼
蒸気ガスタービン及び特殊装置及び水噴射装置の何れか
１以上の出力で駆動する装置を、大中小各種機械とした
ことを特徴とする全動翼蒸気ガスタービン合体機関。313. A device for driving at least one of the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device is a large, medium, or small-sized machine. Moving blade steam gas turbine combined engine. 【請求項３１４】 前記全動翼蒸気タービン及び全動翼
蒸気ガスタービン及び特殊装置及び水噴射装置の何れか
１以上の出力で駆動する装置を、大中小各種艦船とした
ことを特徴とする全動翼蒸気ガスタービン合体機関。314. The large-medium-sized and small-sized ships are used as the device driven by the output of at least one of the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device. Moving blade steam gas turbine combined engine. 【請求項３１５】 前記全動翼蒸気タービン及び全動翼
蒸気ガスタービン及び特殊装置及び水噴射装置の何れか
１以上の出力で駆動する装置を、大中小各種戦車とした
ことを特徴とする全動翼蒸気ガスタービン合体機関。315. A large, medium or small tank is used as the device driven by the output of at least one of the full-blade steam turbine, the full-blade steam gas turbine, the special device, and the water injection device. Moving blade steam gas turbine combined engine. 【請求項３１６】 前記全動翼蒸気タービン及び全動翼
蒸気ガスタービン及び特殊装置及び水噴射装置の何れか
１以上の出力で駆動する装置を、大中小各種戦闘機とし
たことを特徴とする全動翼蒸気ガスタービン合体機関。316. The apparatus driven by any one or more outputs of the full-blade steam turbine, the full-blade steam gas turbine, the special apparatus, and the water injection apparatus is a large, medium, or small fighter. Full rotor steam gas turbine combined engine. 【請求項３１７】 前記全動翼蒸気ガスタービン合体機
関で燃焼させる燃料は、ガソリン・天然ガス・プロパン
ガス・アルコール・メタノール・メタン・水素・軽油・
重油・微粉炭・ゴミガス化燃料・ゴミ微細化燃料・可燃
物の内、何れか１種類にしたことを特徴とする全動翼蒸
気ガスタービン合体機関。317. The fuel burned in the all-blade steam gas turbine integrated engine is gasoline, natural gas, propane gas, alcohol, methanol, methane, hydrogen, light oil,
An all-blade steam gas turbine integrated engine characterized by using any one of heavy oil, pulverized coal, waste gasification fuel, waste miniaturization fuel, and combustibles. 【請求項３１８】 前記全動翼蒸気ガスタービン合体機
関で燃焼させる燃料は、ガソリン・天然ガス・プロパン
ガス・アルコール・メタノール・メタン・水素・軽油・
重油・微粉炭・ゴミガス化燃料・ゴミ微細化燃料・可燃
物の内、何れか２種類にしたことを特徴とする全動翼蒸
気ガスタービン合体機関。318. The fuel burned in the all-blade steam gas turbine coalescence engine is gasoline, natural gas, propane gas, alcohol, methanol, methane, hydrogen, light oil,
An all-blade steam gas turbine integrated engine characterized by using any two types of heavy oil, pulverized coal, waste gasification fuel, waste refinement fuel, and combustibles. 【請求項３１９】 前記全動翼蒸気ガスタービン合体機
関で燃焼させる燃料は、ガソリン・天然ガス・プロパン
ガス・アルコール・メタノール・メタン・水素・軽油・
重油・微粉炭・ゴミガス化燃料・ゴミ微細化燃料・可燃
物の内、何れか３種類以上にしたことを特徴とする全動
翼蒸気ガスタービン合体機関。319. The fuel burned in the all-blade steam gas turbine integrated engine is gasoline, natural gas, propane gas, alcohol, methanol, methane, hydrogen, light oil,
An all-blade steam gas turbine integrated engine characterized by using at least three types of heavy oil, pulverized coal, waste gasification fuel, waste refinement fuel, and combustibles. 【請求項３２０】 前記全動翼蒸気ガスタービン合体機
関で燃焼させる燃料は、その種類を問わないことを特徴
とする全動翼蒸気ガスタービン合体機関。320. The all-blade steam gas turbine united engine, wherein the fuel burned in the all-blade steam gas turbine united engine is of any kind. 【請求項３２１】 前記全動翼蒸気ガスタービン合体機
関の出力で駆動する装置の種類を問わないことを特徴と
する全動翼蒸気ガスタービン合体機関。321. A full-blade steam gas turbine integrated engine, regardless of the type of device driven by the output of the full-blade steam gas turbine integrated engine. 【請求項３２２】 前記全動翼蒸気ガスタービン合体機
関で使用する水に、公害低減地球温暖化防止するため、
物質を混入してＣＯ２等の公害ガスを水に合成溶解容易
にすることを特徴とする全動翼蒸気ガスタービン合体機
関。322. To reduce water pollution used in the all-blade steam gas turbine combined engine to prevent global warming,
An all-blade steam gas turbine integrated engine characterized by mixing substances to facilitate the synthesis and dissolution of pollution gas such as CO2 in water. 【請求項３２３】 前記全動翼蒸気ガスタービン合体機
関で使用する水に、公害低減地球温暖化防止するため、
化学物質を混入してＣＯ２等の公害ガスを水に合成溶解
容易にすることを特徴とする全動翼蒸気ガスタービン合
体機関。323. To reduce water pollution used in the all-blade steam gas turbine combined engine to prevent global warming,
An all- moving blade steam gas turbine integrated engine characterized by mixing chemical substances to facilitate the synthesis and dissolution of pollution gas such as CO2 in water. 【請求項３２４】 前記全動翼蒸気ガスタービン合体機
関で使用する水に、公害低減地球温暖化防止するため、
物質を混入してＣＯ２等の公害ガスを水に合成溶解して
排出することを特徴とする全動翼蒸気ガスタービン合体
機関。324. To reduce pollution in the water used in the all-blade steam gas turbine combined engine to prevent global warming,
An all- moving blade steam gas turbine integrated engine, which mixes substances and synthesizes and dissolves pollution gas such as CO2 in water and discharges it. 【請求項３２５】 前記全動翼蒸気ガスタービン合体機
関で使用する水に、公害低減地球温暖化防止するため、
化学物質を混入してＣＯ２等の公害ガスを水に合成溶解
して排出することを特徴とする全動翼蒸気ガスタービン
合体機関。325. To reduce water pollution used in the all-blade steam gas turbine combined engine to prevent global warming,
An all-blade steam gas turbine integrated engine characterized by mixing a chemical substance with a pollutant gas such as CO2 to dissolve it in water and discharging it. 【請求項３２６】 前記全動翼蒸気ガスタービン合体機
関は、動力伝達装置に摩擦ポンプ（９７）兼用の磁気摩
擦動力伝達装置（１４）を使用することを特徴とする全
動翼蒸気ガスタービン合体機関。326. The all-blade steam gas turbine coalesced engine uses a magnetic friction power transmission device (14) also functioning as a friction pump (97) as a power transmission device. organ. 【請求項３２７】 前記全動翼蒸気ガスタービン合体機
関のタービン翼は、撥水性を良好とすることで、水等と
の間の摩擦損失を低減してタービン翼を動圧反動駆動す
ることを特徴とする全動翼蒸気ガスタービン合体機関。327. The turbine blade of the full-blade steam gas turbine integrated engine is configured to have good water repellency so as to reduce friction loss with water or the like and drive the turbine blade by dynamic pressure reaction. A featured all-blade steam gas turbine integrated engine. 【請求項３２８】 前記全動翼蒸気ガスタービン合体機
関の圧縮翼は、撥水性を良好とすることで、水等との間
の摩擦損失を低減して、効率良く空気圧縮して冷却する
ことを特徴とする全動翼蒸気ガスタービン合体機関。328. The compression blade of the full-blade steam gas turbine coalescing engine has good water repellency to reduce friction loss with water or the like and efficiently perform air compression and cooling. An all-blade steam gas turbine integrated engine characterized by. 【請求項３２９】 前記全動翼圧縮機の撥水性冷却翼
（８７）は、撥水性金属・撥水性物質の被覆・撥水性セ
ラミックス・撥水性加工の、何れかで構成して撥水性を
良好とすることを特徴とする全動翼蒸気ガスタービン合
体機関。329. The water-repellent cooling blade (87) of the full-blade compressor is made of any one of water-repellent metal, coating of water-repellent substance, water-repellent ceramics, and water-repellent finish to have good water repellency. An all-blade steam gas turbine combined engine characterized by the following. 【請求項３３０】 前記タービン翼は、加熱高温・撥水
性金属・撥水性物質の被覆・撥水性セラミックス・撥水
性加工の、何れかで構成して撥水性を良好とすることを
特徴とする全動翼蒸気ガスタービン合体機関。330. The turbine blade is made of any one of heating high temperature, water-repellent metal, coating of water-repellent substance, water-repellent ceramics, and water-repellent finish to improve water repellency. Moving blade steam gas turbine combined engine. 【請求項３３１】 前記撥水性冷却翼（８７）は、撥水
性金属・撥水性物質の被覆・撥水性セラミックス・撥水
性加工の、何れか１以上で構成して撥水性を良好とする
ことを特徴とする全動翼蒸気ガスタービン合体機関。331. The water-repellent cooling blade (87) is made of any one or more of a water-repellent metal, a coating of a water-repellent substance, a water-repellent ceramic, and a water-repellent finish to improve water repellency. A featured all-blade steam gas turbine integrated engine. 【請求項３３２】 前記タービン翼は、加熱高温・撥水
性金属・撥水性物質の被覆・撥水性セラミックス・撥水
性加工の、何れか１以上で構成して撥水性を良好とする
ことを特徴とする全動翼蒸気ガスタービン合体機関。332. The turbine blade is made of any one or more of high temperature heating, water-repellent metal, coating of water-repellent substance, water-repellent ceramics, and water-repellent finish to improve water repellency. Combined full-blade steam gas turbine engine.