FR2640690B1 - Systeme et procede de commande d'un moteur a turbines a gaz - Google Patents

Systeme et procede de commande d'un moteur a turbines a gaz

Info

Publication number
FR2640690B1
FR2640690B1 FR898911037A FR8911037A FR2640690B1 FR 2640690 B1 FR2640690 B1 FR 2640690B1 FR 898911037 A FR898911037 A FR 898911037A FR 8911037 A FR8911037 A FR 8911037A FR 2640690 B1 FR2640690 B1 FR 2640690B1
Authority
FR
France
Prior art keywords
controlling
gas turbine
turbine engine
engine
gas
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.)
Expired - Fee Related
Application number
FR898911037A
Other languages
English (en)
Other versions
FR2640690A1 (fr
Inventor
Michael Solomon Idelchik
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2640690A1 publication Critical patent/FR2640690A1/fr
Application granted granted Critical
Publication of FR2640690B1 publication Critical patent/FR2640690B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Feedback Control In General (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
FR898911037A 1988-12-21 1989-08-18 Systeme et procede de commande d'un moteur a turbines a gaz Expired - Fee Related FR2640690B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/287,231 US4993221A (en) 1988-12-21 1988-12-21 Gas turbine engine control system

Publications (2)

Publication Number Publication Date
FR2640690A1 FR2640690A1 (fr) 1990-06-22
FR2640690B1 true FR2640690B1 (fr) 1994-06-10

Family

ID=23101996

Family Applications (1)

Application Number Title Priority Date Filing Date
FR898911037A Expired - Fee Related FR2640690B1 (fr) 1988-12-21 1989-08-18 Systeme et procede de commande d'un moteur a turbines a gaz

Country Status (5)

Country Link
US (1) US4993221A (fr)
JP (1) JP2755713B2 (fr)
DE (1) DE3926707C2 (fr)
FR (1) FR2640690B1 (fr)
GB (1) GB2226430B (fr)

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US5252860A (en) * 1989-12-11 1993-10-12 Westinghouse Electric Corp. Gas turbine control system having maximum instantaneous load-pickup limiter
DE69024958T2 (de) * 1990-10-25 1996-05-30 Boeing Co Luftgeschwindigkeitsregelsystem für Flugzeugvortriebsregler
US5231823A (en) * 1991-08-22 1993-08-03 General Electric Company Supervisory control system
US5331559A (en) * 1991-09-18 1994-07-19 Alliedsignal Inc. Apparatus for preventing propeller overshoot
US5303542A (en) * 1992-11-16 1994-04-19 General Electric Company Fuel supply control method for a gas turbine engine
US5289685A (en) * 1992-11-16 1994-03-01 General Electric Company Fuel supply system for a gas turbine engine
US5761895A (en) * 1995-08-28 1998-06-09 General Electric Company Transient load controller for gas turbine power generator
US6082092A (en) * 1998-04-08 2000-07-04 General Electric Co. Combustion dynamics control for variable fuel gas composition and temperature based on gas control valve feedback
RU2126903C1 (ru) * 1998-06-09 1999-02-27 Открытое акционерное общество Научно-производственное предприятие "Электронно-гидравлическая автоматика" Способ обнаружения отказов датчиков и контроля исправности объекта
US6250877B1 (en) 2000-07-19 2001-06-26 General Electric Co. Steam turbine controller having method and apparatus for providing variable frequency regulation
US6619027B1 (en) 2000-10-13 2003-09-16 General Electric Company Gas turbine having rotor overspeed and overboost protection
US6578794B1 (en) 2000-11-28 2003-06-17 General Electric Co. Methods and systems for jet engine overthrust protection
US6633828B2 (en) 2001-03-21 2003-10-14 Honeywell International Inc. Speed signal variance detection fault system and method
US6609378B2 (en) * 2002-01-17 2003-08-26 Honeywell International Inc. Energy based fuel control system for gas turbine engines running on multiple fuel types
US7431015B2 (en) * 2006-01-31 2008-10-07 Honeywell International Inc. Fuel metering system proportional bypass valve error compensation system and method
FR2899640B1 (fr) * 2006-04-05 2011-11-25 Eurocopter France Procede et dispositif pour realiser un controle de l'etat de sante d'un turbomoteur d'un giravion bimoteur
US7703272B2 (en) * 2006-09-11 2010-04-27 Gas Turbine Efficiency Sweden Ab System and method for augmenting turbine power output
US7854110B2 (en) 2006-11-16 2010-12-21 Siemens Energy, Inc. Integrated fuel gas characterization system
FR2916419B1 (fr) * 2007-05-22 2010-04-23 Eurocopter France Helicoptere hybride rapide a grande distance franchissable et rotor de sustentation optimise.
JP4831836B2 (ja) * 2007-12-13 2011-12-07 三菱重工業株式会社 ガスタービンの制御方法およびガスタービン発電装置
GB2461925A (en) * 2008-07-18 2010-01-20 Rolls Royce Plc Engine fuel control system
US8321104B2 (en) * 2008-07-18 2012-11-27 Rolls-Royce Plc Control system
US8484981B2 (en) * 2008-08-26 2013-07-16 Siemens Energy, Inc. Integrated fuel gas characterization system
US8768598B2 (en) * 2011-12-26 2014-07-01 Textron Innovations Inc. Dual gain digital engine control
EP3201086B1 (fr) * 2014-10-01 2019-07-31 Sikorsky Aircraft Corporation Gestion de puissance entre un propulseur et un rotor coaxial d'un hélicoptère
FR3031500B1 (fr) * 2015-01-12 2017-01-13 Turbomeca Dispositif et procede de regulation d'un moteur auxiliaire adapte pour fournir une puissance propulsive au rotor d'un helicoptere
US11920521B2 (en) 2022-02-07 2024-03-05 General Electric Company Turboshaft load control using feedforward and feedback control

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3114240A (en) * 1959-09-04 1963-12-17 Bendix Corp Torque indicator and control for turbo-shaft gas turbine engine
US3152444A (en) * 1961-03-01 1964-10-13 Bendix Corp Fuel control apparatus for turbo-shaft engines
GB1205323A (en) * 1968-01-22 1970-09-16 Mini Of Technology Engine fuel supply servo systems
US4188781A (en) * 1978-04-25 1980-02-19 General Electric Company Non-linear dual mode regulator circuit
US4258545A (en) * 1978-06-15 1981-03-31 General Electric Company Optimal control for a gas turbine engine
US4313167A (en) * 1979-07-27 1982-01-26 General Electric Company Thrust control system for a gas turbine engine
US4411595A (en) * 1979-09-19 1983-10-25 General Electric Company Control system for gas turbine engine
US4276744A (en) * 1979-09-19 1981-07-07 General Electric Company Control system for gas turbine engine
US4286324A (en) * 1979-09-24 1981-08-25 Maxwell Ingram Prime mover fuel efficiency control system
GB2065779B (en) * 1979-12-21 1983-09-21 Rolls Royce Gas turbine fuel system
US4423592A (en) * 1980-11-28 1984-01-03 Aviation Electric Ltd. Fuel control system for gas turbine engine
US4593523A (en) * 1980-12-17 1986-06-10 Allied Corporation Method and apparatus for acceleration limiting a gas turbine engine
US4625510A (en) * 1981-04-24 1986-12-02 Bendix Avelex Inc. Stress limiter apparatus for a gas turbine engine
US4449360A (en) * 1981-04-30 1984-05-22 Aviation Electric Ltd. Stall detector and surge prevention feature for a gas turbine engine
US4507915A (en) * 1981-04-30 1985-04-02 Allied Corporation Stall detector and surge prevention feature for a gas turbine engine
US4466526A (en) * 1982-04-16 1984-08-21 Chandler Evans Inc. Helicopter engine control with rotor speed decay anticipator
US4423593A (en) * 1982-04-16 1984-01-03 Chandler Evans Inc. Fuel control for controlling helicopter rotor/turbine acceleration
US4522026A (en) * 1983-02-07 1985-06-11 Pratt & Whitney Canada Inc. Power/torque limiter unit for free turbine type engines
DE3306889A1 (de) * 1983-02-26 1984-08-30 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Einrichtung zur regelung der lastverteilung und der drehzahl von gasturbinenanlagen, insbesondere -triebwerken
US4578945A (en) * 1983-11-10 1986-04-01 Chandler Evans Inc. Overspeed limiter for gas turbine fuel control
US4693077A (en) * 1986-07-18 1987-09-15 General Motors Corporation Closed-loop engine control with feedback torque error compensation
US4716723A (en) * 1986-09-05 1988-01-05 Woodward Governor Company Fuel controls for gas turbine engines

Also Published As

Publication number Publication date
DE3926707C2 (de) 1998-12-24
GB2226430A (en) 1990-06-27
DE3926707A1 (de) 1990-06-28
FR2640690A1 (fr) 1990-06-22
GB8918922D0 (en) 1989-09-27
US4993221A (en) 1991-02-19
JP2755713B2 (ja) 1998-05-25
JPH02188630A (ja) 1990-07-24
GB2226430B (en) 1993-03-17

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Legal Events

Date Code Title Description
BR Restoration of rights
ST Notification of lapse

Effective date: 20080430