FR2273955B1 - - Google Patents

Info

Publication number
FR2273955B1
FR2273955B1 FR7517389A FR7517389A FR2273955B1 FR 2273955 B1 FR2273955 B1 FR 2273955B1 FR 7517389 A FR7517389 A FR 7517389A FR 7517389 A FR7517389 A FR 7517389A FR 2273955 B1 FR2273955 B1 FR 2273955B1
Authority
FR
France
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.)
Expired
Application number
FR7517389A
Other versions
FR2273955A1 (fr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of FR2273955A1 publication Critical patent/FR2273955A1/fr
Application granted granted Critical
Publication of FR2273955B1 publication Critical patent/FR2273955B1/fr
Granted legal-status Critical Current

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
    • F02C9/44—Control of fuel supply responsive to the speed of aircraft, e.g. Mach number control, optimisation of fuel consumption
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F02K1/66—Reversing fan flow using reversing fan blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR7517389A 1974-06-07 1975-06-04 Systeme de controle pour propulseur a ventilateur a pas variable et reversible Granted FR2273955A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/477,533 US3936226A (en) 1974-06-07 1974-06-07 Control system for variable pitch fan propulsor with reverse pitch

Publications (2)

Publication Number Publication Date
FR2273955A1 FR2273955A1 (fr) 1976-01-02
FR2273955B1 true FR2273955B1 (fr) 1979-03-23

Family

ID=23896313

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7517389A Granted FR2273955A1 (fr) 1974-06-07 1975-06-04 Systeme de controle pour propulseur a ventilateur a pas variable et reversible

Country Status (4)

Country Link
US (1) US3936226A (fr)
JP (1) JPS6050971B2 (fr)
FR (1) FR2273955A1 (fr)
GB (1) GB1507167A (fr)

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4206597A (en) * 1976-04-23 1980-06-10 The Boeing Company Fan R.P.M. control loop stabilization using high rotor speed
US4142364A (en) * 1977-07-22 1979-03-06 General Electric Company Back-up control for gas turbine engine
US4275557A (en) * 1978-01-25 1981-06-30 General Electric Company Method and apparatus for controlling thrust in a gas turbine engine
US4506504A (en) * 1983-03-31 1985-03-26 Dresser Industries, Inc Electronic fuel control system for gas turbine
US4671737A (en) * 1984-12-26 1987-06-09 Sundstrand Corporation Blade pitch changing mechanism
US5090196A (en) * 1989-07-21 1992-02-25 The Boeing Company Ducted fan type gas turbine engine power plants
US5161948A (en) * 1991-07-31 1992-11-10 United Technologies Corporation Propulsor pitchlock and feather stop
US5394689A (en) * 1993-09-22 1995-03-07 General Electric Company Gas turbine engine control system having integral flight Mach number synthesis method
DE69400710T2 (de) * 1994-07-01 1997-05-15 Sgs Thomson Microelectronics Fuzzy Logik Steuerungsverfahren bzw. -vorrichtung für einen Induktionsmotor
US6171055B1 (en) * 1998-04-03 2001-01-09 Aurora Flight Sciences Corporation Single lever power controller for manned and unmanned aircraft
US7011498B2 (en) 1998-04-03 2006-03-14 Athena Technologies, Inc. Optimization method for power generation systems
US9506405B2 (en) 1998-04-03 2016-11-29 Rockwell Collins Control Technologies, Inc. Apparatus and method for controlling power generation system
US6318070B1 (en) 2000-03-03 2001-11-20 United Technologies Corporation Variable area nozzle for gas turbine engines driven by shape memory alloy actuators
US6519929B2 (en) 2001-04-30 2003-02-18 Honeywell International, Inc. System and method for controlling the deployment of jet engine thrust reversers
US6526744B2 (en) 2001-04-30 2003-03-04 Honeywell International Inc. System and method for controlling the stowage of jet engine thrust reversers
US6439504B1 (en) 2001-06-15 2002-08-27 Honeywell International, Inc. System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system
US6681559B2 (en) 2001-07-24 2004-01-27 Honeywell International, Inc. Thrust reverser position determination system and method
US6748744B2 (en) * 2001-11-21 2004-06-15 Pratt & Whitney Canada Corp. Method and apparatus for the engine control of output shaft speed
US6684623B2 (en) 2002-02-27 2004-02-03 Honeywell International, Inc. Gearless electric thrust reverser actuators and actuation system incorporating same
US6622963B1 (en) 2002-04-16 2003-09-23 Honeywell International Inc. System and method for controlling the movement of an aircraft engine cowl door
EP1825115A1 (fr) * 2004-12-01 2007-08-29 United Technologies Corporation Regulateur a distance de carburant moteur et regulateur electronique moteur pour moteur a turbine
US8235325B2 (en) 2005-10-04 2012-08-07 United Technologies Corporation Fan variable area nozzle positional measurement system
WO2008045092A1 (fr) * 2006-10-12 2008-04-17 United Technologies Corporation Système de mesure de position pour une buse à section variable de soufflante
EP2074319B1 (fr) * 2006-10-12 2012-08-15 United Technologies Corporation Moteur à turbine à gaz avec tuyère d'éjection variable, ensemble nacelle de ce moteur et procédé de fonctionnement correspondant
WO2008045089A1 (fr) * 2006-10-12 2008-04-17 United Technologies Corporation Profil aérodynamique pour capot de corps central de turbine à gaz
US8127531B2 (en) 2008-11-11 2012-03-06 The Boeing Company Radially translating fan nozzle nacelle
US8959889B2 (en) 2008-11-26 2015-02-24 The Boeing Company Method of varying a fan duct nozzle throat area of a gas turbine engine
US8127532B2 (en) * 2008-11-26 2012-03-06 The Boeing Company Pivoting fan nozzle nacelle
US20110004388A1 (en) * 2009-07-01 2011-01-06 United Technologies Corporation Turbofan temperature control with variable area nozzle
US8291690B1 (en) * 2012-01-31 2012-10-23 United Technologies Corporation Gas turbine engine with variable area fan nozzle positioned for starting
US20140137538A1 (en) * 2012-11-16 2014-05-22 United Technologies Corporation Fast Response Bypass Engine
US10465538B2 (en) 2014-11-21 2019-11-05 General Electric Company Gas turbine engine with reversible fan
US10113508B2 (en) 2014-11-21 2018-10-30 General Electric Company Gas turbine engine and method of assembling the same
US9771878B2 (en) 2015-10-19 2017-09-26 General Electric Company Thrust scheduling method for variable pitch fan engines and turbo-shaft, turbo-propeller engines
US20170145956A1 (en) * 2015-11-20 2017-05-25 General Electric Company Thrust reverse feature control
US10443512B2 (en) 2017-03-31 2019-10-15 Pratt & Whitney Canada Corp. Detection of uncommanded and uncontrollable high thrust events
US10823113B2 (en) 2017-08-21 2020-11-03 Pratt & Whitney Canada Corp. Method and system for limiting power of an engine
CN112761796B (zh) * 2020-12-29 2021-09-28 中国航发控制系统研究所 一种功率闭环控制系统及其方法

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3761042A (en) * 1970-05-16 1973-09-25 Secr Defence Gas turbine engine
US3686860A (en) * 1970-09-25 1972-08-29 Chandler Evans Inc Nozzle control
US3797233A (en) * 1973-06-28 1974-03-19 United Aircraft Corp Integrated control for a turbopropulsion system
US3854287A (en) * 1973-12-26 1974-12-17 United Aircraft Corp Self-trimming control for turbofan engines

Also Published As

Publication number Publication date
JPS518414A (fr) 1976-01-23
JPS6050971B2 (ja) 1985-11-11
FR2273955A1 (fr) 1976-01-02
US3936226A (en) 1976-02-03
GB1507167A (en) 1978-04-12

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Legal Events

Date Code Title Description
ST Notification of lapse