IL62917A - Control system for an augmented turbofan engine - Google Patents

Control system for an augmented turbofan engine

Info

Publication number
IL62917A
IL62917A IL62917A IL6291781A IL62917A IL 62917 A IL62917 A IL 62917A IL 62917 A IL62917 A IL 62917A IL 6291781 A IL6291781 A IL 6291781A IL 62917 A IL62917 A IL 62917A
Authority
IL
Israel
Prior art keywords
control system
turbofan engine
augmented turbofan
augmented
engine
Prior art date
Application number
IL62917A
Other languages
English (en)
Other versions
IL62917A0 (en
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IL62917A0 publication Critical patent/IL62917A0/xx
Publication of IL62917A publication Critical patent/IL62917A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • F02C9/46Emergency fuel control
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • F02C9/32Control of fuel supply characterised by throttling of fuel
    • F02C9/34Joint 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 Turbines (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
IL62917A 1980-07-02 1981-05-20 Control system for an augmented turbofan engine IL62917A (en)

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 (2)

Publication Number Publication Date
IL62917A0 IL62917A0 (en) 1981-07-31
IL62917A true IL62917A (en) 1988-03-31

Family

ID=22597680

Family Applications (1)

Application Number Title Priority Date Filing Date
IL62917A IL62917A (en) 1980-07-02 1981-05-20 Control system for an augmented turbofan engine

Country Status (6)

Country Link
US (1) US4397148A (xx)
JP (1) JPS5738645A (xx)
DE (1) DE3125409A1 (xx)
FR (1) FR2486149B1 (xx)
GB (1) GB2078861B (xx)
IL (1) IL62917A (xx)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
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
US9586690B2 (en) 2013-03-14 2017-03-07 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
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
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
GB2078861B (en) 1983-11-16
US4397148A (en) 1983-08-09
FR2486149B1 (fr) 1985-11-08
JPS5738645A (en) 1982-03-03
GB2078861A (en) 1982-01-13
IL62917A0 (en) 1981-07-31
FR2486149A1 (fr) 1982-01-08
DE3125409A1 (de) 1982-04-15

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