JPS5738645A - Propulsion reinforcing turbo fan engine - Google Patents
Propulsion reinforcing turbo fan engineInfo
- Publication number
- JPS5738645A JPS5738645A JP10071581A JP10071581A JPS5738645A JP S5738645 A JPS5738645 A JP S5738645A JP 10071581 A JP10071581 A JP 10071581A JP 10071581 A JP10071581 A JP 10071581A JP S5738645 A JPS5738645 A JP S5738645A
- Authority
- JP
- Japan
- Prior art keywords
- propulsion
- reinforcing
- turbo fan
- fan engine
- engine
- 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.)
- Pending
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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/46—Emergency fuel control
-
- 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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/32—Control of fuel supply characterised by throttling of fuel
- F02C9/34—Joint control of separate flows to main and auxiliary burners
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/165,159 US4397148A (en) | 1980-07-02 | 1980-07-02 | Control system for an augmented turbofan engine |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5738645A true JPS5738645A (en) | 1982-03-03 |
Family
ID=22597680
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP10071581A Pending JPS5738645A (en) | 1980-07-02 | 1981-06-30 | Propulsion reinforcing turbo fan engine |
Country Status (6)
Country | Link |
---|---|
US (1) | US4397148A (ja) |
JP (1) | JPS5738645A (ja) |
DE (1) | DE3125409A1 (ja) |
FR (1) | FR2486149B1 (ja) |
GB (1) | GB2078861B (ja) |
IL (1) | IL62917A (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2017223212A (ja) * | 2016-06-16 | 2017-12-21 | 早川 秀樹 | エンジンと多目的ファンモーターターボ |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2125185B (en) * | 1982-07-27 | 1986-05-21 | Rolls Royce | Monitoring a control system for a gas turbine engine |
US4794755A (en) * | 1987-05-14 | 1989-01-03 | The United States Of America As Represented By The Secretary Of The Air Force | Back-up control system for F101 engine and its derivatives |
US5197280A (en) * | 1989-03-20 | 1993-03-30 | General Electric Company | Control system and method for controlling a gas turbine engine |
US5279107A (en) * | 1992-06-30 | 1994-01-18 | United Technologies Corporation | Fuel control system with fuel metering valve fault accommodation |
US5768883A (en) * | 1996-01-25 | 1998-06-23 | Ametek Aerospace Products Inc. | Flowrate control sytem and method |
US6568166B2 (en) * | 2000-12-22 | 2003-05-27 | Pratt & Whitney Canada Corp. | Back-up control apparatus for turbo machine |
GB0224039D0 (en) * | 2002-10-16 | 2002-11-27 | Rolls Royce Plc | Control system |
US7454894B2 (en) * | 2004-12-07 | 2008-11-25 | United Technologies Corporation | Supplemental oil cooler airflow for gas turbine engine |
US20070297893A1 (en) * | 2006-06-27 | 2007-12-27 | Winbond Electronics Corporation | Fan speed change control |
US8954228B2 (en) * | 2008-12-30 | 2015-02-10 | Rolls-Royce Corporation | Gas turbine engine failure detection |
FR2990002B1 (fr) * | 2012-04-27 | 2016-01-22 | Snecma | Turbomachine comportant un systeme de surveillance comprenant un module d'engagement d'une fonction de protection de la turbomachine et procede de surveillance |
US8951021B2 (en) | 2013-01-18 | 2015-02-10 | General Electric Company | Dual pump/dual bypass fuel pumping system |
EP2971594B1 (en) * | 2013-03-14 | 2020-01-08 | Rolls-Royce Corporation | Hybrid turbo electric aero-propulsion system control |
FR3023872B1 (fr) * | 2014-07-21 | 2016-07-15 | Sagem Defense Securite | Dispositif de protection contre survitesse d'un moteur d'aeronef |
US11440677B2 (en) * | 2018-11-16 | 2022-09-13 | Rolls-Royce Corporation | Secured backup feature for an embedded system |
US11125169B2 (en) | 2018-12-19 | 2021-09-21 | General Electric Company | Fuel system for heat engine |
FR3130757B1 (fr) * | 2021-12-17 | 2023-12-22 | Safran Helicopter Engines | Procédé de régulation de la vitesse de rotation d’un propulseur d’un groupe propulsif hybride pour aéronef, en situation de panne du système de régulation principal du moteur thermique du groupe propulsif hybride |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1215931A (en) * | 1967-03-11 | 1970-12-16 | Rolls Royce | Improvements in or relating to gas turbine engines |
DE2163344C3 (de) * | 1971-12-21 | 1974-07-04 | Motoren Turbinen Union | Regeleinrichtung für eine Gasturbinenanlage, z. B. ein Kraftfahrzeug- oder Flugtriebwerk |
DE2163804B2 (de) * | 1971-12-22 | 1977-04-21 | Mtu Muenchen Gmbh | Regeleinrichtung fuer eine gasturbinenanlage zum antrieb eines kraftfahrzeugs |
US3834361A (en) * | 1972-08-23 | 1974-09-10 | Bendix Corp | Back-up fuel control system |
US3987620A (en) * | 1973-07-31 | 1976-10-26 | Fiat Termomeccanica E Turbogas S.P.A. | Device for controlling gas turbine engines |
US3854287A (en) * | 1973-12-26 | 1974-12-17 | United Aircraft Corp | Self-trimming control for turbofan engines |
US4136517A (en) * | 1976-07-06 | 1979-01-30 | General Electric Company | Thrust control system for a gas turbine engine |
US4128995A (en) * | 1976-10-18 | 1978-12-12 | General Electric Company | Method and apparatus for stabilizing an augmenter system |
US4159625A (en) * | 1977-02-01 | 1979-07-03 | United Technologies Corporation | Control for gas turbine engine |
US4128208A (en) * | 1977-07-11 | 1978-12-05 | General Electric Company | Exhaust nozzle flap seal arrangement |
-
1980
- 1980-07-02 US US06/165,159 patent/US4397148A/en not_active Expired - Lifetime
-
1981
- 1981-05-18 GB GB8115223A patent/GB2078861B/en not_active Expired
- 1981-05-20 IL IL62917A patent/IL62917A/xx unknown
- 1981-06-27 DE DE19813125409 patent/DE3125409A1/de not_active Withdrawn
- 1981-06-30 JP JP10071581A patent/JPS5738645A/ja active Pending
- 1981-07-02 FR FR8113033A patent/FR2486149B1/fr not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2017223212A (ja) * | 2016-06-16 | 2017-12-21 | 早川 秀樹 | エンジンと多目的ファンモーターターボ |
Also Published As
Publication number | Publication date |
---|---|
DE3125409A1 (de) | 1982-04-15 |
IL62917A0 (en) | 1981-07-31 |
FR2486149B1 (fr) | 1985-11-08 |
FR2486149A1 (fr) | 1982-01-08 |
US4397148A (en) | 1983-08-09 |
GB2078861A (en) | 1982-01-13 |
GB2078861B (en) | 1983-11-16 |
IL62917A (en) | 1988-03-31 |
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