FR2460391B1 - - Google Patents

Info

Publication number
FR2460391B1
FR2460391B1 FR8014412A FR8014412A FR2460391B1 FR 2460391 B1 FR2460391 B1 FR 2460391B1 FR 8014412 A FR8014412 A FR 8014412A FR 8014412 A FR8014412 A FR 8014412A FR 2460391 B1 FR2460391 B1 FR 2460391B1
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
FR8014412A
Other versions
FR2460391A1 (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.)
Smiths Group PLC
Original Assignee
Smiths Group PLC
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 Smiths Group PLC filed Critical Smiths Group PLC
Publication of FR2460391A1 publication Critical patent/FR2460391A1/fr
Application granted granted Critical
Publication of FR2460391B1 publication Critical patent/FR2460391B1/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
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/04—Purpose of the control system to control acceleration (u)

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Control Of Turbines (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Supercharger (AREA)
FR8014412A 1979-06-29 1980-06-27 Circuit de reglage du debit de carburant d'un moteur a turbine a gaz Granted FR2460391A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7922683A GB2052805B (en) 1979-06-29 1979-06-29 Gas-turbine engine control

Publications (2)

Publication Number Publication Date
FR2460391A1 FR2460391A1 (fr) 1981-01-23
FR2460391B1 true FR2460391B1 (fr) 1984-11-16

Family

ID=10506181

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8014412A Granted FR2460391A1 (fr) 1979-06-29 1980-06-27 Circuit de reglage du debit de carburant d'un moteur a turbine a gaz

Country Status (4)

Country Link
US (1) US4344141A (fr)
DE (1) DE3023550A1 (fr)
FR (1) FR2460391A1 (fr)
GB (1) GB2052805B (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4488236A (en) * 1982-04-16 1984-12-11 United Technologies Corporation Helicopter cruise fuel conserving engine control
US4470118A (en) * 1982-04-19 1984-09-04 Chandler Evans Inc. Gas turbine engine fuel control
US4532763A (en) * 1983-01-28 1985-08-06 General Electric Company Isochronous gas turbine speed control
CA1246717A (fr) * 1983-08-01 1988-12-13 James J. Howlett Rehausseur de facteur de charge pour aeronef a voilure tournante
US4783957A (en) * 1986-12-23 1988-11-15 Sundstrand Corporation Fuel control circuit for a turbine engine
US4912642A (en) * 1987-09-03 1990-03-27 The Boeing Company Coordinated engine autothrottle
GB8800904D0 (en) * 1988-01-15 1988-02-17 Rolls Royce Plc Fuel control system
GB2218537B (en) * 1988-05-11 1993-02-17 Rolls Royce Plc Engine control
US4998202A (en) * 1989-05-19 1991-03-05 United Technologies Corporation Helicopter, high rotor load speed enhancement
US5029441A (en) * 1989-09-20 1991-07-09 United Technologies Corporation Dynamic compensation to n-dot schedules
US5212943A (en) * 1991-10-08 1993-05-25 Sundstrand Corporation Reduced thermal stress turbine starting strategy
DE4139529C2 (de) * 1991-11-30 1994-03-24 Daimler Benz Ag Verfahren zur Steuerung einer Luftmenge zu der einer Gasturbine in Abhängigkeit von Last und Drehzahl zugeführten Brennstoffmenge
FR2704905B1 (fr) * 1993-05-06 1995-06-09 Snecma Turbomachine comportant un regulateur secondaire du debit de son alimentation en carburant.
US5596871A (en) * 1995-05-31 1997-01-28 Alliedsignal Inc. Deceleration fuel control system for a turbine engine
US6098008A (en) * 1997-11-25 2000-08-01 Caterpillar Inc. Method and apparatus for determining fuel control commands for a cruise control governor system
US6487490B1 (en) 1999-05-26 2002-11-26 General Electric Company Speed modification system for gas turbine engine to allow trimming of excess
US6568166B2 (en) 2000-12-22 2003-05-27 Pratt & Whitney Canada Corp. Back-up control apparatus for turbo machine
DE10302074A1 (de) 2003-01-21 2004-07-29 Rolls-Royce Deutschland Ltd & Co Kg Fehlerdetektionslogik für Triebwerke
US7010399B2 (en) * 2003-11-24 2006-03-07 The Boeing Company Methods and apparatus for fuel control using inertial measurement data
IL305614B1 (en) 2012-10-11 2024-05-01 Nanocomposix Inc Compositions of silver nanoparticle coating and methods
CN103557082B (zh) * 2013-10-25 2015-12-30 中国航空动力机械研究所 一种发动机燃油供给装置和控制方法
US20180058462A1 (en) * 2016-08-23 2018-03-01 Honeywell International Inc. Gas turbine engine compressor surge avoidance control system and method
US10801361B2 (en) 2016-09-09 2020-10-13 General Electric Company System and method for HPT disk over speed prevention
US11643981B2 (en) * 2021-08-30 2023-05-09 Pratt & Whitney Canada Corp. System and method for controlling fuel flow to an aircraft engine during start

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1470757A (en) * 1973-04-27 1977-04-21 Lucas Industries Ltd Fuel control systems for gas turbine engines
US4077204A (en) * 1973-10-23 1978-03-07 Nissan Motor Company, Limited Control system for a gas turbine engine
JPS5534292B2 (fr) * 1974-06-13 1980-09-05
GB1520412A (en) * 1974-07-09 1978-08-09 Lucas Industries Ltd Gas turbine engine fuel control systems
DE2702774C3 (de) * 1977-01-24 1980-12-18 Bodenseewerk Geraetetechnik Gmbh, 7770 Ueberlingen Vorrichtung zur Drehzahlregelung von Turbo-Luftstrahltriebwerken
US4142364A (en) * 1977-07-22 1979-03-06 General Electric Company Back-up control for gas turbine engine

Also Published As

Publication number Publication date
GB2052805B (en) 1983-03-09
DE3023550A1 (de) 1981-01-15
FR2460391A1 (fr) 1981-01-23
GB2052805A (en) 1981-01-28
US4344141A (en) 1982-08-10
DE3023550C2 (fr) 1990-02-08

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Legal Events

Date Code Title Description
ST Notification of lapse