FR2279934A1 - Commande electronique de combustible pour moteur a turbine a gaz - Google Patents

Commande electronique de combustible pour moteur a turbine a gaz

Info

Publication number
FR2279934A1
FR2279934A1 FR7523102A FR7523102A FR2279934A1 FR 2279934 A1 FR2279934 A1 FR 2279934A1 FR 7523102 A FR7523102 A FR 7523102A FR 7523102 A FR7523102 A FR 7523102A FR 2279934 A1 FR2279934 A1 FR 2279934A1
Authority
FR
France
Prior art keywords
gas turbine
fuel control
turbine engines
electronic fuel
electronic
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.)
Granted
Application number
FR7523102A
Other languages
English (en)
French (fr)
Other versions
FR2279934B1 (OSRAM
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
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 Lucas Industries Ltd filed Critical Lucas Industries Ltd
Publication of FR2279934A1 publication Critical patent/FR2279934A1/fr
Application granted granted Critical
Publication of FR2279934B1 publication Critical patent/FR2279934B1/fr
Granted legal-status Critical Current

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
    • F02C9/28Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/04Purpose of the control system to control acceleration (u)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/04Purpose of the control system to control acceleration (u)
    • F05D2270/042Purpose of the control system to control acceleration (u) by keeping it below damagingly high values
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/10Purpose of the control system to cope with, or avoid, compressor flow instabilities
    • F05D2270/101Compressor surge or stall

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 Eletrric Generators (AREA)
  • Electrical Control Of Air Or Fuel Supplied To Internal-Combustion Engine (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
FR7523102A 1974-07-24 1975-07-24 Commande electronique de combustible pour moteur a turbine a gaz Granted FR2279934A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB32637/74A GB1520882A (en) 1974-07-24 1974-07-24 Electronic fuel control for a gas turbine engine

Publications (2)

Publication Number Publication Date
FR2279934A1 true FR2279934A1 (fr) 1976-02-20
FR2279934B1 FR2279934B1 (OSRAM) 1980-09-26

Family

ID=10341742

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7523102A Granted FR2279934A1 (fr) 1974-07-24 1975-07-24 Commande electronique de combustible pour moteur a turbine a gaz

Country Status (6)

Country Link
US (1) US4040250A (OSRAM)
JP (1) JPS6018818B2 (OSRAM)
DE (1) DE2532817C2 (OSRAM)
FR (1) FR2279934A1 (OSRAM)
GB (1) GB1520882A (OSRAM)
IT (1) IT1041014B (OSRAM)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2465880A1 (fr) * 1979-09-21 1981-03-27 Lucas Industries Ltd Systeme de controle d'alimentation en carburant d'un moteur a turbine a gaz
FR2486589A1 (fr) * 1980-07-10 1982-01-15 Lucas Industries Ltd Dispositif de regulation de l'alimentation en carburant d'un moteur de turbine a gaz
EP0053547A1 (en) * 1980-11-28 1982-06-09 AVIATION ELECTRIC Limited Fuel control system for gas turbine engine
EP0082785A3 (en) * 1981-12-21 1983-07-27 The Bendix Corporation Fuel control system for gas turbine engine

Families Citing this family (36)

* Cited by examiner, † Cited by third party
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US4206597A (en) * 1976-04-23 1980-06-10 The Boeing Company Fan R.P.M. control loop stabilization using high rotor speed
US4217754A (en) * 1977-01-22 1980-08-19 Bodenseewerk Geratetechnik Gmbh Apparatus for controlling the rotary speed in turbo-jet engines for aircraft
DE2702774C3 (de) * 1977-01-24 1980-12-18 Bodenseewerk Geraetetechnik Gmbh, 7770 Ueberlingen Vorrichtung zur Drehzahlregelung von Turbo-Luftstrahltriebwerken
GB2032142B (en) * 1978-10-02 1982-11-03 Lucas Industries Ltd Fuel control for a multi-engine gas turbine installation
JPS55131532A (en) * 1979-03-29 1980-10-13 Nissan Motor Co Ltd Fuel controller for gas turbine engine
JPS55161921A (en) * 1979-06-04 1980-12-16 Nissan Motor Co Ltd Fuel control device for gas turbine engine
JPS5641423A (en) * 1979-09-10 1981-04-18 Nissan Motor Co Ltd Fuel controller for gas turbine engine
US4593523A (en) * 1980-12-17 1986-06-10 Allied Corporation Method and apparatus for acceleration limiting a gas turbine engine
US4432201A (en) * 1981-01-14 1984-02-21 Aviation Electric Ltd. Acceleration limit reset
US4442667A (en) * 1981-01-14 1984-04-17 Aviation Electric Ltd. Acceleration limit reset
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
US4417440A (en) * 1981-05-12 1983-11-29 Aviation Electric Ltd. Fuel control apparatus for a gas turbine engine
US4422289A (en) * 1981-05-12 1983-12-27 Aviation Electric Ltd. Fuel control apparatus for a gas turbine engine
US4423593A (en) * 1982-04-16 1984-01-03 Chandler Evans Inc. Fuel control for controlling helicopter rotor/turbine acceleration
US4470257A (en) * 1982-04-30 1984-09-11 Westinghouse Electric Corp. Isochronous and droop speed control for a combustion turbine
GB2126382B (en) * 1982-08-10 1986-01-08 Nissan Motor Gas turbine engine control system
JPS5924942U (ja) * 1982-08-10 1984-02-16 日産自動車株式会社 ガスタ−ビンエンジンの制御装置
US4532763A (en) * 1983-01-28 1985-08-06 General Electric Company Isochronous gas turbine speed control
US4672806A (en) * 1983-01-28 1987-06-16 General Electric Company Isochronous gas turbine speed control
US4651518A (en) * 1984-12-18 1987-03-24 United Technologies Corporation Transient derivative scheduling control system
GB2228977B (en) * 1985-08-02 1990-11-21 Lucas Ind Plc Running control for a gas turbine engine
JPS6233112U (OSRAM) * 1985-08-16 1987-02-27
JPH0792016B2 (ja) * 1986-06-09 1995-10-09 三菱電機株式会社 内燃機関用燃料噴射弁駆動回路の故障検出回路
US4884397A (en) * 1988-04-29 1989-12-05 United Technologies Corporation Control system topping loop
US4845943A (en) * 1988-04-29 1989-07-11 United Technologies Corporation Control method for topping loop
US5180923A (en) * 1990-11-01 1993-01-19 Westinghouse Electric Corp. Method and apparatus for downline load rejection sensing in a gas turbine control system
GB9410760D0 (en) * 1994-05-27 1994-07-27 Rolls Royce Plc Gas turbine engine fuel control system
US20050274115A1 (en) * 2004-06-15 2005-12-15 Pearce Kevin P Method and Apparatus for Prevention of Compressor Stall and Combustion Flameout in a Turbine Engine
US8090456B2 (en) * 2008-11-03 2012-01-03 United Technologies Corporation System and method for design and control of engineering systems utilizing component-level dynamic mathematical model
US8131384B2 (en) * 2008-11-03 2012-03-06 United Technologies Corporation Design and control of engineering systems utilizing component-level dynamic mathematical model with multiple-input multiple-output estimator
US8352152B2 (en) * 2009-02-10 2013-01-08 Honeywell International Inc. System, method, apparatus and computer program product for providing improved engine control
US8315741B2 (en) * 2009-09-02 2012-11-20 United Technologies Corporation High fidelity integrated heat transfer and clearance in component-level dynamic turbine system control
US8668434B2 (en) * 2009-09-02 2014-03-11 United Technologies Corporation Robust flow parameter model for component-level dynamic turbine system control
US11649038B2 (en) * 2020-07-10 2023-05-16 Pratt & Whitney Canada Corp. Hybrid electric powerplant (HEP) control architecture

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB962801A (en) * 1959-07-17 1964-07-01 Dehavilland Aircraft Improvements in or relating to engine control systems
US3174529A (en) * 1960-05-31 1965-03-23 Garrett Corp Control system
US3098356A (en) * 1960-10-20 1963-07-23 Sperry Rand Corp Fuel control system for gas turbine engines
GB1090143A (en) * 1965-04-07 1967-11-08 Hawker Siddeley Dynamics Ltd Improvements in or relating to electrical control systems for engines
GB1271818A (en) * 1969-09-18 1972-04-26 Rolls Royce Improvements in or relating to electronic control means for a closed loop control system
US3688504A (en) * 1970-11-27 1972-09-05 Gen Electric Bypass valve control
DE2064340C3 (de) * 1970-12-29 1973-12-06 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Regeleinrichtung für eine Gasturbi nenanlage
US3868625A (en) * 1972-12-20 1975-02-25 United Aircraft Corp Surge indicator for turbine engines
GB1470757A (en) * 1973-04-27 1977-04-21 Lucas Industries Ltd Fuel control systems for gas turbine engines
US3852958A (en) * 1973-09-28 1974-12-10 Gen Electric Stall protector system for a gas turbine engine
GB1519144A (en) * 1974-07-09 1978-07-26 Lucas Industries Ltd Electronic fuel control for a gas turbine engine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2465880A1 (fr) * 1979-09-21 1981-03-27 Lucas Industries Ltd Systeme de controle d'alimentation en carburant d'un moteur a turbine a gaz
FR2486589A1 (fr) * 1980-07-10 1982-01-15 Lucas Industries Ltd Dispositif de regulation de l'alimentation en carburant d'un moteur de turbine a gaz
EP0053547A1 (en) * 1980-11-28 1982-06-09 AVIATION ELECTRIC Limited Fuel control system for gas turbine engine
EP0082785A3 (en) * 1981-12-21 1983-07-27 The Bendix Corporation Fuel control system for gas turbine engine

Also Published As

Publication number Publication date
FR2279934B1 (OSRAM) 1980-09-26
DE2532817A1 (de) 1976-02-12
IT1041014B (it) 1980-01-10
JPS5149314A (en) 1976-04-28
US4040250A (en) 1977-08-09
JPS6018818B2 (ja) 1985-05-13
GB1520882A (en) 1978-08-09
DE2532817C2 (de) 1983-12-15

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Legal Events

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ST Notification of lapse