JP6241814B2 - Rotary engine - Google Patents

Rotary engine Download PDF

Info

Publication number
JP6241814B2
JP6241814B2 JP2015221648A JP2015221648A JP6241814B2 JP 6241814 B2 JP6241814 B2 JP 6241814B2 JP 2015221648 A JP2015221648 A JP 2015221648A JP 2015221648 A JP2015221648 A JP 2015221648A JP 6241814 B2 JP6241814 B2 JP 6241814B2
Authority
JP
Japan
Prior art keywords
engine
air
combustion chamber
rotary engine
water jacket
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
JP2015221648A
Other languages
Japanese (ja)
Other versions
JP2017082751A (en
Inventor
鈴木 克彦
克彦 鈴木
Original Assignee
鈴木 克彦
克彦 鈴木
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 鈴木 克彦, 克彦 鈴木 filed Critical 鈴木 克彦
Priority to JP2015221648A priority Critical patent/JP6241814B2/en
Publication of JP2017082751A publication Critical patent/JP2017082751A/en
Application granted granted Critical
Publication of JP6241814B2 publication Critical patent/JP6241814B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Output Control And Ontrol Of Special Type Engine (AREA)

Description

ロータリーエンジンを搭載した自動車や2輪車、電車、飛行機船舶等の乗り物や発電機、ポンプ、コンプレッサーなど。Vehicles such as automobiles, motorcycles, trains, airplane ships, etc. equipped with rotary engines, generators, pumps, compressors, etc.

近年、益々自動車のエンジンは小型化、高出力化、低燃費が求められ、エンジンの高効率化が求められている。In recent years, more and more automobile engines are required to have smaller size, higher output, and lower fuel consumption, and higher efficiency of the engine is required.

発明が解決しようとする課題Problems to be solved by the invention

ロータリーエンジンは4サイクルエンジンと比較して小型高出力と言う特徴を持つが、燃費が悪いと言う欠点を持つ。エンジンの冷却を高めてエンジンの温度を低くすると線膨張係数によって混合気が収縮するため、混合気の圧縮工程で圧力が低下し、ポンピングロスが下がるが、混合気が爆発して膨張するときにロータリーエンジンのハウジングに熱を奪われて爆発後の燃焼ガスの温度が低下し、ロータリーエンジンの燃焼室の圧力が低下し、ローターを押す力が低下してエンジン出力が低下する。つまり冷却ロスが大きくなり、出力や燃費が低下し、実行効率が低下する。本発明はロータリーエンジンのハウジングの温度の制御によって実行効率の高いロータリーエンジンを提供する。A rotary engine has a feature of small size and high output as compared with a four-cycle engine, but has a disadvantage of poor fuel consumption. Increasing engine cooling and lowering engine temperature causes the air-fuel mixture to contract due to the coefficient of linear expansion, which reduces the pressure during the air-fuel compression process and reduces pumping loss. The heat of the rotary engine is deprived of heat, the temperature of the combustion gas after the explosion decreases, the pressure of the combustion chamber of the rotary engine decreases, the force pushing the rotor decreases, and the engine output decreases. That is, the cooling loss increases, the output and fuel consumption decrease, and the execution efficiency decreases. The present invention provides a rotary engine with high execution efficiency by controlling the temperature of the housing of the rotary engine.

課題を解決するための手段Means for solving the problem

4サイクルエンジンは同一シリンダー内で混合気を圧縮し燃焼してピストンを押し下げてエンジン出力が発生する。しかしロータリーエンジンは混合気の圧縮室と燃焼室が分かれているため、ロータリーエンジンの圧縮室の部分はハウジングのウォータージャケットに冷却水を流して冷却して混合気の圧力を下げてポンピングロスを低下させ、燃焼室の部分はハウジングのウォータージャケットに排気ガスを流して排気熱で燃焼室を加熱し、燃焼室内の燃焼ガスの温度低下を抑制することによって燃焼室内の冷却損失による圧力低下を抑制して高いエンジン出力が得られる。The 4-cycle engine compresses and burns the air-fuel mixture in the same cylinder and pushes down the piston to generate engine output. However, since the rotary engine has a separate compression chamber and combustion chamber, the compression chamber portion of the rotary engine is cooled by flowing cooling water through the water jacket of the housing to lower the pressure of the mixture and lower the pumping loss. The combustion chamber part controls the pressure drop due to the cooling loss in the combustion chamber by flowing the exhaust gas through the water jacket of the housing and heating the combustion chamber with exhaust heat to suppress the temperature drop of the combustion gas in the combustion chamber. High engine output.

発明の効果Effect of the invention

ロータリーエンジンの実行効率が向上し、燃費とエンジン出力向上を同時に改善でき、4サイクルエンジンよりも小型高出力、低燃費エンジンが得られる。The execution efficiency of the rotary engine is improved, and the fuel efficiency and the engine output can be improved at the same time. A compact, high output and low fuel consumption engine can be obtained compared to the 4-cycle engine.

本発明のロータリーエンジンの断面概念図である。1はハウジング、2はローター、3はエキセントリックシャフト、4はスパークプラグ、5は排気ポート、6は吸気ポート、7は燃焼室、8は圧縮室、9は加熱ジャケット、10は水冷ジャケットである。1のハウジングの中の壁に沿って反時計回りにローター2が回転し、ローター2が自転しながら公転することによってエキセントリックシャフト3が反時計回りに回転し、外部に動力を出力する。ローターの回転によって圧縮室8の体積が拡大するときに吸気ポート6から混合気が入り、次に燃焼室の体積が狭くなるとともに混合気が圧縮され、混合気の体積が小さくなって高圧になった時にスパークプラグ4が点火し、混合気が燃焼する。混合気が燃焼して高温になることによって圧力が上昇し、燃焼室7の体積が膨張しながらローター2が進角し、ローター2のギアを反してエキセントリックシャフト3に回転力が伝わる。そして燃焼室の体積が収縮するときに排気ポート5から燃焼ガスが排出され、また吸気ポート6から次の混合気の吸気が始まる。圧縮室8を冷却するため、10の水冷ジャケットに外部の空気によって冷やされた流体が流れる。一方、燃焼室7の温度を高温に保つため、加熱ジャケット9に排気熱によって加熱した流体が流れる。It is a section conceptual diagram of the rotary engine of the present invention. 1 is a housing, 2 is a rotor, 3 is an eccentric shaft, 4 is a spark plug, 5 is an exhaust port, 6 is an intake port, 7 is a combustion chamber, 8 is a compression chamber, 9 is a heating jacket, and 10 is a water cooling jacket. The rotor 2 rotates counterclockwise along the wall in the housing 1, and the eccentric shaft 3 rotates counterclockwise as the rotor 2 revolves while rotating to output power to the outside. When the volume of the compression chamber 8 expands due to the rotation of the rotor, the air-fuel mixture enters from the intake port 6, and then the volume of the combustion chamber decreases and the air-fuel mixture is compressed. The spark plug 4 ignites and the air-fuel mixture burns. When the air-fuel mixture burns and becomes high temperature, the pressure rises, the volume of the combustion chamber 7 expands, the rotor 2 advances, and the rotational force is transmitted to the eccentric shaft 3 against the rotor 2 gear. When the volume of the combustion chamber contracts, the combustion gas is discharged from the exhaust port 5 and the intake of the next air-fuel mixture starts from the intake port 6. In order to cool the compression chamber 8, a fluid cooled by external air flows through 10 water cooling jackets. On the other hand, in order to keep the temperature of the combustion chamber 7 at a high temperature, the fluid heated by the exhaust heat flows through the heating jacket 9.

Claims (1)

ウォータジャッケット付ハウジングとローターで構成されたロータリーエンジンの混合気圧縮側のウォータージャケットに冷却水、クーラント、空気などの気体又は液体からなる冷却流体を流し、燃焼室側のウォータージャケットには排気ガス、又は排気ガスで加熱した液体又は気体からなる加熱流体を流し、エンジンを始動して10分以上経過した時のエンジン運転時に、ハウジングの混合気圧縮側のウォータージャケットを流れる冷却流体に対して燃焼室側のウォータージャケットを流れる加熱流体の温度が少なくとも70℃以上高くすることを特徴とするエンジンとこのエンジンを使ったシステム.    A cooling fluid composed of a gas or a liquid such as cooling water, coolant, air, etc. flows through a water jacket on the air-fuel mixture compression side of a rotary engine composed of a housing with a water jacket and a rotor, and exhaust gas, Or a combustion chamber for cooling fluid flowing through the water jacket on the air-fuel mixture compression side of the housing when the engine is operating when a heated fluid made of liquid or gas heated with exhaust gas is flown and the engine is started for 10 minutes or more An engine characterized in that the temperature of the heated fluid flowing through the water jacket on the side is increased by at least 70 ° C. and a system using the engine.
JP2015221648A 2015-10-23 2015-10-23 Rotary engine Active JP6241814B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2015221648A JP6241814B2 (en) 2015-10-23 2015-10-23 Rotary engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2015221648A JP6241814B2 (en) 2015-10-23 2015-10-23 Rotary engine

Publications (2)

Publication Number Publication Date
JP2017082751A JP2017082751A (en) 2017-05-18
JP6241814B2 true JP6241814B2 (en) 2017-12-06

Family

ID=58710493

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015221648A Active JP6241814B2 (en) 2015-10-23 2015-10-23 Rotary engine

Country Status (1)

Country Link
JP (1) JP6241814B2 (en)

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55108215U (en) * 1979-01-23 1980-07-29
JPS59153923A (en) * 1983-02-21 1984-09-01 Toyota Motor Corp Adiabatic engine
JPS60194156U (en) * 1984-06-04 1985-12-24 トヨタ自動車株式会社 Cylinder bore warming promotion and cooling device

Also Published As

Publication number Publication date
JP2017082751A (en) 2017-05-18

Similar Documents

Publication Publication Date Title
EP1788221A2 (en) Dual six-stroke self-cooling internal cobustion engine
US8033264B2 (en) Rotary engine
RU2015126486A (en) AIR COOLED ROTARY ENGINE
RU2342546C2 (en) Electric generator based on piston-free engine with remote combustion chamber
RU2605143C1 (en) Aircraft bypass turbojet engine two high pressure turbines cooling system
US20090205331A1 (en) Piston based double compounding engine
JP6241814B2 (en) Rotary engine
CN210686064U (en) Pressure storage type engine
US2420136A (en) Six cycle engine
RU2008138792A (en) COMBINED ATOMIC FORCING AIRCRAFT ENGINE
US2293548A (en) Pressure gas generator
GB968029A (en) Rotary piston internal combustion engine
ES2848320B2 (en) rotary internal combustion engine
KR20060080910A (en) Rotary. engine
CN100453779C (en) Turbine rotor engine
US1233951A (en) Explosion-engine.
RU2013114637A (en) ROTARY-TURBINE INTERNAL COMBUSTION ENGINE WITH EXTERNAL COMBUSTION CHAMBER, STEAM PHASE AND WITH OPPORTUNITY TO WORK ON THE HYDROGEN-OXYGEN MIXTURE, UNDER THE CLOSED CYCLE IN MODE OF THE MODE
ES1243790U (en) Rotary internal combustion engine (Machine-translation by Google Translate, not legally binding)
US1362541A (en) Internal-combustion engine
RU2528811C2 (en) Stirling engine
US10514017B2 (en) Internal combustion engine with igniter cooling sleeve
RU2578241C2 (en) Rotary internal combustion engine
WO2013177613A1 (en) Rotary combustion engine
CN110645050A (en) Pressure storage type engine and acting method
US1133058A (en) Internal-combustion gas-turbine.

Legal Events

Date Code Title Description
A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20170228

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20170725

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20170909

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20171024

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20171029

R150 Certificate of patent or registration of utility model

Ref document number: 6241814

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250