JP7424674B1 - Expansion/rotary engine - Google Patents
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- JP7424674B1 JP7424674B1 JP2022167210A JP2022167210A JP7424674B1 JP 7424674 B1 JP7424674 B1 JP 7424674B1 JP 2022167210 A JP2022167210 A JP 2022167210A JP 2022167210 A JP2022167210 A JP 2022167210A JP 7424674 B1 JP7424674 B1 JP 7424674B1
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- 238000004880 explosion Methods 0.000 claims abstract description 64
- 239000002360 explosive Substances 0.000 claims abstract description 7
- 239000000567 combustion gas Substances 0.000 claims description 17
- 239000007789 gas Substances 0.000 claims description 17
- 238000005192 partition Methods 0.000 claims description 3
- 230000002093 peripheral effect Effects 0.000 claims description 2
- 238000002485 combustion reaction Methods 0.000 abstract description 17
- 238000000034 method Methods 0.000 abstract description 13
- 239000000446 fuel Substances 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 abstract 1
- 230000006835 compression Effects 0.000 description 8
- 238000007906 compression Methods 0.000 description 8
- 238000002347 injection Methods 0.000 description 8
- 239000007924 injection Substances 0.000 description 8
- 230000000694 effects Effects 0.000 description 2
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 238000003306 harvesting Methods 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
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Abstract
【課題】爆発行程で発生した運動エネルギーのさらなる回転エネルギーへの変換効率化を図り爆音を軽減した内燃機関を提供する。
【解決手段】軸芯回転のローターの1回転で、4工程が同時に連続稼働しながら、複数の回転機能の追加により、運動エネルギーの効率的な採取により燃費の向上を図り、爆発の騒音軽減を実現した。
【選択図】図4
An object of the present invention is to provide an internal combustion engine that improves the efficiency of converting kinetic energy generated during an explosion stroke into rotational energy and reduces explosive noise.
[Solution] With one revolution of the rotor rotating on its axis, four processes are operated simultaneously and continuously, and by adding multiple rotation functions, efficient collection of kinetic energy improves fuel efficiency and reduces explosion noise. It was realized.
[Selection diagram] Figure 4
Description
母筒状体内のローターの回転軸と子筒状体のローターの回転軸を一直線状にして筒状体を重ねて一体化し、燃焼ガスの排気口または排出口と導入口を連通させて燃焼エネルギーの効率化により燃費の向上を図るロータリーエンジンに関する。
また、燃焼用気体を加圧して筒状体内に送り込む場合は、吸入を注入と呼び変える場合もある。
燃焼用気体の爆発は、燃焼であり膨張でもある
The rotational axis of the rotor in the mother cylinder and the rotational axis of the rotor in the child cylinder are aligned, and the cylinders are overlapped and integrated, and the combustion gas exhaust port or exhaust port and inlet are communicated to generate combustion energy. Related to rotary engines that aim to improve fuel efficiency by increasing efficiency.
Furthermore, when pressurizing combustion gas and sending it into the cylindrical body, suction may be called injection.
The explosion of combustion gas is both combustion and expansion.
ロータリーエンジンの、特公平7-30706や、特願2022-8978は燃焼行程で発生した運動エネルギーの未利用部分はそのまま爆音と共に排出されていた For rotary engines, the unused portion of the kinetic energy generated in the combustion process is directly emitted with an explosive sound in Patent Publication No. 7-30706 and Patent Application No. 2022-8978.
それは、前記内燃機関の燃焼行程で発生した運動エネルギーの未利用部分と爆音が構造的仕組みにより、そのまま排出せざるを得なかったためである。 This is because the unused portion of kinetic energy and loud noise generated during the combustion stroke of the internal combustion engine have to be emitted as is due to the structural mechanism.
先願のロータリーエンジンの、特公平7-30706はローターの回転時に該羽根の先端とロータリー内燃機関の内周壁曲面が乖離するのを防ぐために設けた羽根底のばねや燃焼圧取入孔に燃焼圧を導入して羽根の基端から羽根を押し上げる構成であり、特願2022-8978の羽根は、該羽根の先端部から内周曲面方向への縦方向、あるいは両側の側壁方向への横方向の突出部がロータリーエンジン内に周回掘削したガイド溝と周回自在に密接嵌合させることにより、ロータリーエンジン内は内周曲面と該羽根先端が常に密接周回するものであった The prior application for the rotary engine, JP-B-7-30706, uses a spring in the bottom of the blade and a combustion pressure intake hole provided to prevent the tips of the blades from separating from the curved surface of the inner peripheral wall of the rotary internal combustion engine when the rotor rotates. The blade is configured to push up the blade from the base end of the blade by introducing pressure, and the blade of Japanese Patent Application No. 2022-8978 is configured to push up the blade from the tip of the blade in the vertical direction toward the inner circumferential curved surface, or in the lateral direction toward the side walls on both sides. By tightly fitting the protruding part of the vane into a guide groove drilled in the rotary engine so that it can rotate freely, the inner curved surface and the tip of the vane always circulate closely in the rotary engine.
いずれも単一の筒状体形状の燃焼行程で発生したエネルギーを燃焼爆発時に回転エネルギーに一部変換する以外、未利用の運動エネルギーはそのまま外部に廃棄され、またエンジン内で爆音が軽減されることはなかったが、内燃機関の爆発行程で発生した運動エネルギーのさらなる回転エネルギーへの変換効率化を
図ることにより、爆音も軽減されるべきであった
In both cases, the energy generated during the combustion process of a single cylindrical body is partially converted into rotational energy during the combustion explosion, and the unused kinetic energy is discarded to the outside as is, and the explosion noise inside the engine is reduced. Although this was not the case, efforts were made to improve the efficiency of converting the kinetic energy generated during the internal combustion engine's explosion stroke into rotational energy.
The explosion noise should have been reduced by
円筒形の内周壁を有する筒状体の内半径の一部を大きくしたスペースのハウジングを設け、別設したローターの回転軸からの放射状方向に穿設した数本の羽根溝にハウジングの内周壁に向かって前進後退してハウジング内を区分けする羽根を装着したローターをそのハウジング内に挿嵌して、ローターの回転方向のそのスペースの始端部に点火素子を設けて前進した羽根の先端で区分けされた爆発室内に連続して補給される爆発用の加圧気体が、点火素子の点火により爆発して該羽根の先端を押してローターを回転させ、そのスペースの終端部に排気口を設定して爆発排気スペースとして、該筒状体の両側を側壁により閉鎖した筒状体を母筒状体と称し、
円筒形の内周壁を有する他の筒状体の内半径の一部を一か所大きくしたスペースを、その始端部に導入口と終端部に排出口のある爆発延長スペースとしたハウジングを設け、前記様の羽根溝のローターをそのハウジング内に挿嵌して、該筒状体の両側を側壁により閉鎖した一つ以上の筒状体を子筒状体と称し、
それらローターの回転軸を一直線状に連結して筒状体を重ねて一体化し、排気口または排出口と導入口が連通したロータリーエンジンとする。
A housing with a space in which a part of the inner radius of a cylindrical body having a cylindrical inner circumferential wall is enlarged is provided, and several blade grooves bored in a radial direction from the rotating shaft of a separately installed rotor are connected to the inner circumferential wall of the housing. A rotor equipped with vanes that move forward and backward to partition the inside of the housing is inserted into the housing, and an ignition element is provided at the starting end of the space in the direction of rotation of the rotor to divide the space at the tips of the blades that move forward. The pressurized gas for explosion that is continuously supplied into the explosion chamber explodes when the ignition element ignites, pushing the tip of the blade and rotating the rotor, and an exhaust port is set at the end of the space. A cylindrical body whose both sides are closed by side walls as an explosion exhaust space is called a base cylindrical body,
A housing is provided in which a part of the inner radius of another cylindrical body having a cylindrical inner circumferential wall is enlarged by one place is used as an explosion extension space with an inlet at the starting end and an outlet at the terminal end, One or more cylindrical bodies in which the rotor with the blade grooves as described above is inserted into its housing and both sides of the cylindrical body are closed by side walls are referred to as child cylindrical bodies,
The rotating shafts of these rotors are connected in a straight line, and the cylindrical bodies are stacked and integrated to form a rotary engine in which the exhaust port or the exhaust port and the inlet port communicate with each other.
前記爆発室内に連続して補給される爆発用の加圧気体とは、特公平7-30706や、特願2022-8978にもいう筒状体内において、ハウジング内の注入、圧縮、爆発、排気、の各工程のうち、注入工程で注入口から爆発用の気体として注入され、圧縮行程で加圧圧縮されて爆発室に移送されて連続して補給されて爆発用となる加圧気体を言い、
あるいはその筒状体内においての注入口を無くして注入、圧縮の行程を省略し、筒状体外部の爆発用の加圧気体の収容装置と爆発室を連通させ、その爆発室側の連通口に設置した噴出弁がその加圧気体を爆発室内にローターの回転と同期して一定量噴出させては停止し、その一定量噴出分を点火素子が点火爆発させる、などして連続補給される爆発用の加圧気体をいうのである。
The pressurized gas for explosion that is continuously replenished into the explosion chamber means injection, compression, explosion, exhaust, Among these processes, pressurized gas is injected as an explosive gas from the injection port in the injection process, compressed under pressure in the compression stroke, transferred to the explosion chamber, and continuously replenished for explosion purposes.
Alternatively, the injection port in the cylindrical body can be eliminated to omit the injection and compression steps, and the explosion chamber can be communicated with the pressurized gas storage device for explosion outside the cylindrical body, and the communication port on the side of the explosion chamber can be connected to the explosion chamber. An explosion that is continuously replenished by an installed blowout valve that blows out a fixed amount of pressurized gas into the explosion chamber in synchronization with the rotation of the rotor, then stops, and then an ignition element ignites and explodes the fixed amount of gas ejected. It refers to pressurized gas for use.
そうして、
爆発行程での爆発エネルギーをローターの羽根の前記先端部分が受けて回転する母筒状体のローターの回転軸と、子筒状体のローターの回転軸を一直線状
に連結して筒状体を重ねて一体化するにおいて、母筒状体内でローターを回転させるエネルギーとなり得なかった残余の爆発エネルギーは排気口に連通する子筒状体の導入口から子筒状体内の爆発延長スペースに導入されてそのスペースのローターの羽根の前進した先端部分が受けて子筒状体のローターを回転させるもので、母筒状体に連通する子筒状体と、さらに追加の子筒状体を同様に排出口と導入口を連結増設すれば、さらなる回転エネルギー採取の効率化が図られ、また、
消音マフラーの如く爆発延長スペースの延長増加による消音効果で、それら問題解決に寄与するのである。
Then,
A cylindrical body is formed by connecting in a straight line the rotation axis of the rotor of the mother cylindrical body, which rotates when the tip portion of the blade of the rotor receives the explosion energy during the explosion stroke, and the rotation axis of the rotor of the child cylindrical body. When stacking and integrating, the remaining explosion energy that could not be used as energy to rotate the rotor in the mother cylinder is introduced into the explosion extension space in the child cylinder from the inlet of the child cylinder that communicates with the exhaust port. The advanced tip of the rotor blade in that space is received and rotates the rotor of the child cylindrical body, and the child cylindrical body communicating with the mother cylindrical body and additional child cylindrical bodies are similarly connected. By connecting and expanding the outlet and inlet, you can further improve the efficiency of harvesting rotational energy.
Like a sound-deadening muffler, the sound-deadening effect by increasing the length of the explosion extension space contributes to solving these problems.
本発明は、爆発延長スペースのある子筒状体を付加することにより爆発行程を延長する効果を生み、爆発行程で発生した運動エネルギーを、排気口や排出口と導入口が連通して隣接の爆発延長スペースにおいても爆発膨張ガス、すなわち運動エネルギーを導入してローターを回転させるので、母筒状体の爆発排気スペース部分の回転範囲に限られることなく、爆発行程で発生した運動エネルギーの利用採取範囲を拡大させて燃費の向上を図り、前記増設付加態様次第では母筒状体のローターの1回転以上の利用採取範囲も可能となり、例えば後記図面の3枚羽の母筒状体に、子筒状体を三個付加した場合、ハウジング円周の凡そ3分の4、1回転以上の利用採取範囲となり、
また、2枚羽の母筒状体の場合には筒状体外部の加圧気体の収容装置と爆発室を連通させて爆発室内に爆発用の加圧気体を連続して補給して爆発させ、慣性によりローターを回転させ、以上、爆発行程で発生した運動エネルギーの有効的存在が消滅するか、取り付け外形の収納容量の許す限り、増設付加を検討できる。
The present invention has the effect of extending the explosion stroke by adding a sub-cylindrical body with an explosion extension space, and the kinetic energy generated in the explosion stroke is transferred to the adjacent cylinder by communicating the exhaust port and the exhaust port with the inlet. Since the explosion expansion gas, that is, kinetic energy, is introduced into the explosion extension space to rotate the rotor, the kinetic energy generated during the explosion stroke can be used and harvested without being limited to the rotation range of the explosion exhaust space of the base cylinder. In order to improve fuel efficiency by expanding the range, depending on the above-mentioned expansion and addition mode, it is possible to use the collection range of more than one rotation of the rotor of the main cylinder. When three cylindrical bodies are added, the usable collection range is approximately 4/3 of the circumference of the housing, which is more than one rotation.
In addition, in the case of a two-blade base cylinder, the pressurized gas storage device outside the cylinder is connected to the explosion chamber, and the explosion chamber is continuously supplied with pressurized gas for explosion. , the rotor is rotated by inertia, and as long as the effective existence of the kinetic energy generated in the explosion stroke disappears, or as long as the storage capacity of the installed external shape allows, you can consider adding an extension.
加えて、燃焼室で発生する爆発膨張音は排気口や排出口と導入口が連通して延長する各燃焼室工程が消音の効果をもたらし、各筒状体内で爆発膨張音を閉じ込めることにより、回転エネルギーとなって爆発膨張の音を弱化させ、一方、自動車の消音マフラーや銃のサイレンサー装置においては運動エネルギー効率に寄与することはないのである。 In addition, the explosion and expansion noise generated in the combustion chamber is silenced by each combustion chamber process where the exhaust port and the exhaust port are connected and extended, and by trapping the explosion and expansion noise within each cylindrical body. It turns into rotational energy and weakens the sound of the explosion and expansion, but on the other hand, it does not contribute to the kinetic energy efficiency of automobile mufflers or gun silencers.
先願の、燃焼室における燃料の爆発による膨張圧を単体のローターの羽根
の前進先端部分のみが受け、ローターを回転させて回転エネルギーとしていたが、単体ゆえに排気口から多くの未利用エネルギーが廃棄されていた。この
事象はレシプロエンジン等、従来の内燃機関にも惹起しており、その解決のため、数多の提案がなされていた。
また、騒音となる燃焼による爆発音を軽減すべく従来既存の消音マフラーが付
随される場合、運動エネルギーに対する抵抗要素としてその効率を低下させていた
In the previous application, only the advancing tip of the blade of a single rotor received the expansion pressure caused by the explosion of fuel in the combustion chamber, causing the rotor to rotate and converting it into rotational energy, but because it was a single rotor, a lot of unused energy was discarded from the exhaust port. It had been. this
This phenomenon has also occurred in conventional internal combustion engines such as reciprocating engines, and many proposals have been made to solve the problem.
In addition, when conventional mufflers are attached to reduce the explosion noise caused by combustion, they reduce their efficiency as a resistance element to kinetic energy.
従来のピストン運動型のレシプロエンジンは注入、圧縮、爆発、排気の4工程を1サイクルとして同一のシリンダーを共用し、クランクロッドの進退運動により該工程が順次稼働するため、各4分の1が稼働工程となり、残り4分の3の工程は稼働待機態勢としての非効率性があるため、シリンダー数を増加して駆動力を強化する場合があり、また同一のシリンダーで燃料の注入工程と爆発工程を行えば、噴霧状燃料や水素等の燃焼用気体状の引火性の強い素材に対し安全上の脆弱性が常に危惧されるに対し、本発明のロータリーエンジンは前記各工程室を独立遮断して安全性を高めてその4工程は同時に稼働するため、3枚羽を装着したローターの場合、ローターの3分の1回転が1サイクルとなり、4枚羽を装着したローターの場合よりも膨張行程の円周距離は長く、1 回転ではその羽根の数と同数の各サイクルが実現し、いずれの枚数でも待機態勢のない効率的な駆動力により、エンジンの小型化と軽量化が実現する。 Conventional piston motion type reciprocating engines share the same cylinder with the four steps of injection, compression, explosion, and exhaust as one cycle, and each step is operated sequentially by the forward and backward movement of the crank rod, so one quarter of each cycle is The remaining three-quarters of the process is inefficient as it is on standby, so the number of cylinders may be increased to strengthen the driving force, and the same cylinder is used for the fuel injection process and the explosion process. When processes are carried out, there is always a concern about safety vulnerabilities due to highly flammable materials in the form of atomized fuel or combustion gases such as hydrogen.However, the rotary engine of the present invention isolates each of the process chambers independently. This increases safety and the four processes operate simultaneously, so in the case of a rotor equipped with three blades, one third rotation of the rotor is one cycle, and the expansion stroke is shorter than in the case of a rotor equipped with four blades. The circumferential distance of the blade is long, and in one rotation, each cycle is the same as the number of blades, and regardless of the number of blades, efficient driving force without standby allows the engine to be made smaller and lighter.
従来、バンケル型ロータリーエンジンと呼称する内部の三角状ローターの偏心運動により駆動力を発生させる内燃機関はその偏心駆動態様により、クランクレスレシプロエンジンと称されるべきであり、一方、本発明のロータリーエンジンは偏心ロスのない有効性を実現するのである。 Conventionally, an internal combustion engine that generates driving force by the eccentric movement of an internal triangular rotor, called a Wankel rotary engine, should be called a crankless reciprocating engine due to its eccentric drive mode.On the other hand, the rotary engine of the present invention The engine achieves effectiveness without eccentric losses.
本発明の実施の一例の形態を図1、図2、図3、図4に基づいて説明する。
なお、図面において、排気口や排出口や導入口の連通形状の一方が長径となるのは、筒状体のローターの回転軸方向に長く平行の開口部とすることにより、排気口や排出口や導入口、等開口部を筒状体の形状に合わせて大きくして工程気体の速やかな通過を可能とするためである。
また、本実施例においては母筒状体と子筒状体のローターや外周を同径サイズとしているが、異径サイズとすることによりローターの回転軸方向の筒状体の母筒状体と子筒状体の輪切り形状の幅を調整し本発明のロータリーエンジンの設置環境に合わせた荷姿とする場合もある。
An embodiment of the present invention will be described based on FIGS. 1, 2, 3, and 4.
In addition, in the drawings, one of the communication shapes of the exhaust port, discharge port, and inlet has a long diameter, because the opening is long and parallel to the rotational axis direction of the cylindrical rotor. This is because openings such as the inlet and the inlet are made large to match the shape of the cylindrical body to allow process gas to pass through quickly.
In addition, in this embodiment, the rotors and outer circumferences of the parent cylindrical body and the child cylindrical body are made of the same diameter size, but by making them different diameter sizes, In some cases, the width of the sliced shape of the child cylindrical body may be adjusted to provide a packaging style that matches the installation environment of the rotary engine of the present invention.
1ロータリーエンジン
2母筒状体
3子筒状体
4子筒状体
5羽根
8点火素子
21母筒状体ローター
23羽根溝
24母筒状体ハウジング
26排気口
27導入口
31子筒状体ローター
32子筒状体ハウジング
33子筒状体羽根溝
36排出口
37導入口
41子筒状体ローター
46排出口
47導入口
51先端部
53先端部
71点線
221爆発排気スペース
223吸入圧縮スペース
324爆発延長スペース
423爆発延長スペース
2211爆発室
A回転軸
B方向
C方向
D方向
E方向
F方向
1
23
71
A rotation axis B direction
C direction D direction
E direction
F direction
Claims (1)
母筒状体ローター21の回転方向のその爆発排気スペース221の始端部に点火素子8を設け、
前進した羽根5の先端で区分けされた爆発室内に連続して補給される爆発用の加圧気体が爆発して、該羽根の先端を押して母筒状体ローター21を回転させ、
その爆発排気スペース221の終端部に排気口26を設定し、該母筒状体ハウジング24の両側を側壁により閉鎖した筒状体とし、
円筒形の内周壁を有する他の子筒状体3の内半径の一か所を大きくした爆発延長スペース324の、始端部に爆発排気スペース221からの爆発気体の導入口37と、終端部に爆発気体の排出口36を設けた子筒状体ハウジング32を設け、
前記と同様の回転軸からの放射状方向に穿設した数本の羽根溝に子筒状体ハウジング32の内周壁に向かって前進後退して子筒状体ハウジング32内を区分けする羽根5を装着した子筒状体ローター31を、その子筒状体ハウジング32内に挿嵌して、該子筒状体ハウジング32の両側を側壁により閉鎖した一つ以上の筒状体を設け、
それら母筒状体ローター21の回転軸と、前記一つ以上の子筒状体ローター31の回転軸とを一直線状に連結し、
母筒状体ハウジング24の中心軸と、子筒状体ハウジング32の中心軸とを一直線状に連結して、筒状体を重ねて一体化し、
母筒状体ハウジング24への燃燃焼用気体の導入口27から、子筒状体ハウジング32からの一つ以上の子筒状体の排出口までを、連通されるようにしたロータリーエンジン1。
A part of the inner radius of the base cylinder body 2 having a cylindrical inner circumferential wall is enlarged to provide a base cylinder body housing 24 in which an explosion exhaust space 221 is formed, and a rotating shaft of a separately provided base cylinder body rotor 21 is provided. A base cylindrical body rotor equipped with vanes 5 which move forward and backward toward the inner circumferential wall of the base cylindrical body housing 24 to partition the inside of the base cylindrical body housing 24 in several vane grooves bored in the radial direction from the base cylindrical body rotor. 21 into its base cylindrical body housing 24,
An ignition element 8 is provided at the starting end of the explosion exhaust space 221 in the rotational direction of the base cylindrical body rotor 21,
Explosive pressurized gas continuously supplied into the explosion chamber divided by the tips of the advanced blades 5 explodes, pushing the tips of the blades and rotating the base cylindrical rotor 21,
An exhaust port 26 is set at the end of the explosion exhaust space 221, and the base cylindrical body housing 24 is formed into a cylindrical body with both sides closed by side walls.
The explosion extension space 324, which has a cylindrical inner peripheral wall and has a larger inner radius at one point, has an inlet 37 for introducing explosive gas from the explosion exhaust space 221 at the starting end, and an inlet 37 for the explosive gas from the explosion exhaust space 221 at the terminal end. A child cylindrical body housing 32 is provided with an explosive gas outlet 36,
The vanes 5 which move forward and backward toward the inner circumferential wall of the secondary cylindrical body housing 32 to partition the inside of the secondary cylindrical body housing 32 are attached to several blade grooves bored in the radial direction from the rotating shaft as described above. The child cylindrical body rotor 31 is inserted into the child cylindrical body housing 32, and one or more cylindrical bodies are provided in which both sides of the child cylindrical body housing 32 are closed by side walls,
The rotation axis of the mother cylindrical body rotor 21 and the rotation axis of the one or more child cylindrical body rotors 31 are connected in a straight line,
The central axis of the mother cylindrical body housing 24 and the central axis of the child cylindrical body housing 32 are connected in a straight line, and the cylindrical bodies are stacked and integrated,
A rotary engine 1 in which an inlet 27 for introducing combustion gas into a mother cylindrical body housing 24 and an outlet for one or more child cylindrical bodies from a child cylindrical body housing 32 are communicated with each other.
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