JPS5189917A - - Google Patents
Info
- Publication number
- JPS5189917A JPS5189917A JP50153196A JP15319675A JPS5189917A JP S5189917 A JPS5189917 A JP S5189917A JP 50153196 A JP50153196 A JP 50153196A JP 15319675 A JP15319675 A JP 15319675A JP S5189917 A JPS5189917 A JP S5189917A
- Authority
- JP
- Japan
- 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
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/22—Fuel supply systems
- F02C7/236—Fuel delivery systems comprising two or more pumps
- F02C7/2365—Fuel delivery systems comprising two or more pumps comprising an air supply system for the atomisation of fuel
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/543,092 US3971210A (en) | 1975-01-22 | 1975-01-22 | Start-up compressed air system for gas turbine engines |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS5189917A true JPS5189917A ( ) | 1976-08-06 |
JPS597016B2 JPS597016B2 (ja) | 1984-02-16 |
Family
ID=24166545
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP50153196A Expired JPS597016B2 (ja) | 1975-01-22 | 1975-12-22 | ガスタ−ビンエンジンヨウシドウアツシユククウキソウチ |
Country Status (6)
Country | Link |
---|---|
US (1) | US3971210A ( ) |
JP (1) | JPS597016B2 ( ) |
CA (1) | CA1031170A ( ) |
FR (1) | FR2298694A1 ( ) |
GB (1) | GB1530330A ( ) |
IT (1) | IT1052479B ( ) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4189914A (en) * | 1978-06-19 | 1980-02-26 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Supercritical fuel injection system |
EP0014075A1 (en) * | 1979-01-22 | 1980-08-06 | The Garrett Corporation | Fuel atomising arrangements in gas turbine engines |
JPS5915635A (ja) * | 1982-07-15 | 1984-01-26 | Hitachi Ltd | 噴霧空気系統を有するガスタ−ビン |
US5012646A (en) * | 1988-11-28 | 1991-05-07 | Machen, Inc. | Turbine engine having combustor air precooler |
US5136837A (en) * | 1990-03-06 | 1992-08-11 | General Electric Company | Aircraft engine starter integrated boundary bleed system |
US5143329A (en) * | 1990-06-01 | 1992-09-01 | General Electric Company | Gas turbine engine powered aircraft environmental control system and boundary layer bleed |
US5125597A (en) * | 1990-06-01 | 1992-06-30 | General Electric Company | Gas turbine engine powered aircraft environmental control system and boundary layer bleed with energy recovery system |
US5137230A (en) * | 1991-06-04 | 1992-08-11 | General Electric Company | Aircraft gas turbine engine bleed air energy recovery apparatus |
WO1998020243A1 (en) * | 1996-11-08 | 1998-05-14 | Northern Research & Engineering Corporation | Turbine engine with turbocompressor for supplying atomizing fluid to turbine engine fuel system |
US6557337B1 (en) * | 1998-09-25 | 2003-05-06 | Alm Development, Inc. | Gas turbine engine |
US6324867B1 (en) * | 1999-06-15 | 2001-12-04 | Exxonmobil Oil Corporation | Process and system for liquefying natural gas |
GB9924545D0 (en) * | 1999-10-19 | 1999-12-22 | Rolls Royce Plc | Vehicle main and auxiliary power units |
JP3593488B2 (ja) * | 2000-02-25 | 2004-11-24 | 株式会社日立製作所 | ガスタービン |
US6499303B1 (en) * | 2001-04-18 | 2002-12-31 | General Electric Company | Method and system for gas turbine power augmentation |
US20040226299A1 (en) * | 2003-05-12 | 2004-11-18 | Drnevich Raymond Francis | Method of reducing NOX emissions of a gas turbine |
BR112012005612A2 (pt) * | 2009-09-13 | 2016-06-21 | Lean Flame Inc | pré-misturador de entrada para aparelho de combustão |
US9086018B2 (en) | 2010-04-23 | 2015-07-21 | Hamilton Sundstrand Corporation | Starting a gas turbine engine to maintain a dwelling speed after light-off |
US10480418B2 (en) * | 2012-10-26 | 2019-11-19 | Powerphase Llc | Gas turbine energy supplementing systems and heating systems, and methods of making and using the same |
MX362906B (es) | 2012-10-26 | 2019-02-25 | Powerphase Llc | Sistemas de complemento de energía de turbina de gas y sistemas de calentamiento y métodos de hacer y usar los mismos. |
US10030580B2 (en) * | 2014-04-11 | 2018-07-24 | Dynamo Micropower Corporation | Micro gas turbine systems and uses thereof |
CN105986846A (zh) * | 2015-02-27 | 2016-10-05 | 福建三钢闽光股份有限公司 | 一种余热余能回收联合发电机组的对接式及空载冷却装置 |
CN107630754A (zh) * | 2017-08-17 | 2018-01-26 | 俞平 | 燃气压缩机支持燃气轮机点火 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR972400A ( ) * | 1951-01-29 | |||
FR878970A (fr) * | 1941-02-03 | 1943-02-10 | Brown | Dispositif pour le démarrage et la marche à vide de turbines à gaz à combustion continue et à refroidissement par air |
US2303381A (en) * | 1941-04-18 | 1942-12-01 | Westinghouse Electric & Mfg Co | Gas turbine power plant and method |
DE768006C (de) * | 1941-06-21 | 1955-05-05 | Messerschmitt Boelkow Blohm | Heissstrahltriebwerk zum Vortrieb von Luftfahrzeugen |
US2394253A (en) * | 1941-07-10 | 1946-02-05 | Nettel Frederick | Air expansion power system |
US2813231A (en) * | 1956-01-17 | 1957-11-12 | Westinghouse Electric Corp | Over-pressure protection of pipe lines |
US2976683A (en) * | 1958-09-08 | 1961-03-28 | Gen Motors Corp | Gas turbine fuel system with regenerator temperature compensation |
FR1261487A (fr) * | 1960-06-09 | 1961-05-19 | Rover Co Ltd | Système de mise en marche pour moteur à turbine à gaz |
US3072058A (en) * | 1961-08-18 | 1963-01-08 | Socony Mobil Oil Co Inc | Pipe line control system |
US3577965A (en) * | 1969-08-08 | 1971-05-11 | Chandler Evans Inc | Fuel atomization system having a compressor drive means |
US3581493A (en) * | 1969-12-12 | 1971-06-01 | Avco Corp | Air assist for fuel injector |
US3722218A (en) * | 1970-12-04 | 1973-03-27 | Parker Hannifin Corp | Air boost fuel atomizing system |
-
1975
- 1975-01-22 US US05/543,092 patent/US3971210A/en not_active Expired - Lifetime
- 1975-11-03 CA CA238,902A patent/CA1031170A/en not_active Expired
- 1975-12-02 IT IT52496/75A patent/IT1052479B/it active
- 1975-12-22 JP JP50153196A patent/JPS597016B2/ja not_active Expired
-
1976
- 1976-01-07 GB GB554/76A patent/GB1530330A/en not_active Expired
- 1976-01-20 FR FR7601374A patent/FR2298694A1/fr active Granted
Also Published As
Publication number | Publication date |
---|---|
US3971210A (en) | 1976-07-27 |
FR2298694A1 (fr) | 1976-08-20 |
IT1052479B (it) | 1981-06-20 |
GB1530330A (en) | 1978-10-25 |
CA1031170A (en) | 1978-05-16 |
FR2298694B1 ( ) | 1982-09-17 |
JPS597016B2 (ja) | 1984-02-16 |