JPS57165631A - Rotary engine - Google Patents
Rotary engineInfo
- Publication number
- JPS57165631A JPS57165631A JP56050918A JP5091881A JPS57165631A JP S57165631 A JPS57165631 A JP S57165631A JP 56050918 A JP56050918 A JP 56050918A JP 5091881 A JP5091881 A JP 5091881A JP S57165631 A JPS57165631 A JP S57165631A
- Authority
- JP
- Japan
- Prior art keywords
- blade part
- compression groove
- providing
- communicated
- rotor
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/02—Methods of operating
-
- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rotary Pumps (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
PURPOSE:To reduce mechanical loss of an engine and increse its efficiency, by circumferentially providing a compression groove to a true round shaped rotor, providing a press contact piston in the compression groove, providing a blade part in the periphery of the rotor and providing a jet port, communicated to the blade part, in a combustion chamber. CONSTITUTION:A compression groove 16 is circumferentially provided to a true round shaped rotor 10, and a protrusive part 18 is formed to divide the compression groove 16. An in-out movable press contact piston 28 is provided in the vicinity of an intake port 22 in the compression groove 16. An explosion chamber 32 is formed to the end of a high pressure gas passage 30 and communicated by a check valve 38. A blade part 40 is provided in a necessary peripheral surface of the rotor 10, and a jet port 34, communicated to the blade part 40, is provided in the explosion chamber 32. A shock wave, generaed by compresed air and fuel of a fuel injection device 36 in the explosion chamber 32, collides against the blade part 40 from the jet port 34 to apply rotary energy. In this way, an energy saving rotary engine of high efficiency can be obtained.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP56050918A JPS57165631A (en) | 1981-04-03 | 1981-04-03 | Rotary engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP56050918A JPS57165631A (en) | 1981-04-03 | 1981-04-03 | Rotary engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS57165631A true JPS57165631A (en) | 1982-10-12 |
JPS6133975B2 JPS6133975B2 (en) | 1986-08-05 |
Family
ID=12872166
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP56050918A Granted JPS57165631A (en) | 1981-04-03 | 1981-04-03 | Rotary engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS57165631A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1988006226A1 (en) * | 1987-02-16 | 1988-08-15 | Jyuichi Umino | Gas turbine |
JP2005520085A (en) * | 2002-03-14 | 2005-07-07 | ニュートン・プロパルション・テクノロジーズ・リミテッド | Gas turbine engine system |
US7621116B2 (en) | 2003-08-31 | 2009-11-24 | Newton Propulsion Technologies, Ltd. | Gas turbine engine system |
-
1981
- 1981-04-03 JP JP56050918A patent/JPS57165631A/en active Granted
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1988006226A1 (en) * | 1987-02-16 | 1988-08-15 | Jyuichi Umino | Gas turbine |
JP2005520085A (en) * | 2002-03-14 | 2005-07-07 | ニュートン・プロパルション・テクノロジーズ・リミテッド | Gas turbine engine system |
US8109074B2 (en) | 2002-03-14 | 2012-02-07 | Newton Propuslion Technologies | Gas turbine engine system |
US7621116B2 (en) | 2003-08-31 | 2009-11-24 | Newton Propulsion Technologies, Ltd. | Gas turbine engine system |
Also Published As
Publication number | Publication date |
---|---|
JPS6133975B2 (en) | 1986-08-05 |
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