GB1548713A - Gas turbine engine fuel control system - Google Patents

Gas turbine engine fuel control system

Info

Publication number
GB1548713A
GB1548713A GB21411/76A GB2141176A GB1548713A GB 1548713 A GB1548713 A GB 1548713A GB 21411/76 A GB21411/76 A GB 21411/76A GB 2141176 A GB2141176 A GB 2141176A GB 1548713 A GB1548713 A GB 1548713A
Authority
GB
United Kingdom
Prior art keywords
control system
gas turbine
turbine engine
fuel control
engine fuel
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
Application number
GB21411/76A
Other languages
English (en)
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 GB1548713A publication Critical patent/GB1548713A/en
Expired 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
    • F02C9/32—Control of fuel supply characterised by throttling of fuel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
GB21411/76A 1975-05-29 1976-05-24 Gas turbine engine fuel control system Expired GB1548713A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/581,752 US4186556A (en) 1975-05-29 1975-05-29 Compressor bleed biased acceleration schedule

Publications (1)

Publication Number Publication Date
GB1548713A true GB1548713A (en) 1979-07-18

Family

ID=24326431

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21411/76A Expired GB1548713A (en) 1975-05-29 1976-05-24 Gas turbine engine fuel control system

Country Status (7)

Country Link
US (1) US4186556A (enExample)
JP (1) JPS5941012B2 (enExample)
CA (1) CA1054385A (enExample)
DE (1) DE2623945C2 (enExample)
FR (1) FR2312657A1 (enExample)
GB (1) GB1548713A (enExample)
IT (1) IT1060564B (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4157010A (en) * 1977-06-03 1979-06-05 General Electric Company Gas turbine engine with power modulation capability
US4606189A (en) * 1984-03-29 1986-08-19 General Electric Company Fuel control
US4627789A (en) * 1984-09-19 1986-12-09 Avco Corporation Apparatus method for calibrating and setting compressor air bleed valve schedules
US5226287A (en) * 1991-07-19 1993-07-13 General Electric Company Compressor stall recovery apparatus
US5205116A (en) * 1991-07-19 1993-04-27 General Electric Company Compressor stall recovery apparatus
US6935120B2 (en) * 2002-05-09 2005-08-30 General Electric Company Approach to extending life of gas turbine engine
US7762084B2 (en) * 2004-11-12 2010-07-27 Rolls-Royce Canada, Ltd. System and method for controlling the working line position in a gas turbine engine compressor
US7762078B2 (en) * 2006-09-13 2010-07-27 Aerojet-General Corporation Nozzle with temperature-responsive throat diameter
US9611752B2 (en) 2013-03-15 2017-04-04 General Electric Company Compressor start bleed system for a turbine system and method of controlling a compressor start bleed system
US10077720B2 (en) * 2015-04-17 2018-09-18 Honda Motor Co., Ltd. Control apparatus for a gas-turbine aeroengine

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2653446A (en) * 1948-06-05 1953-09-29 Lockheed Aircraft Corp Compressor and fuel control system for high-pressure gas turbine power plants
FR1078776A (fr) * 1952-06-17 1954-11-23 Rolls Royce Perfectionnements aux moteurs à turbine à gaz
GB750147A (en) * 1953-01-13 1956-06-13 Lucas Industries Ltd Jet-propulsion prime movers
NL107023C (enExample) * 1955-03-17 1963-08-15
US2930520A (en) * 1957-05-01 1960-03-29 United Aircraft Corp Compressor bleed control
US2978166A (en) * 1957-05-28 1961-04-04 Gen Motors Corp Compressor bleed control
US3080712A (en) * 1959-02-05 1963-03-12 Continental Aviat & Eng Corp Compressor anti-surge control for a gas turbine engine
US3006145A (en) * 1959-10-14 1961-10-31 Gen Motors Corp Antisurge control using compressor bleed
US3137210A (en) * 1960-07-21 1964-06-16 United Aircraft Corp Pressure ratio bleed control
US3172259A (en) * 1962-03-02 1965-03-09 Avco Corp Variable geometry control for gas turbine engines
US3255586A (en) * 1962-09-12 1966-06-14 Dresser Ind Gas turbine capable of rapidly accepting or rejecting a load with minimum speed deviation
US3513899A (en) * 1968-03-29 1970-05-26 United Aircraft Corp Fuel control deceleration mode
US3533238A (en) * 1968-12-23 1970-10-13 Gen Electric Inlet control system
US3727400A (en) * 1971-06-10 1973-04-17 Curtiss Wright Corp Gas turbine air compressor and control therefor
US3797233A (en) * 1973-06-28 1974-03-19 United Aircraft Corp Integrated control for a turbopropulsion system
US3849020A (en) * 1973-09-13 1974-11-19 Bendix Corp Fluidic compressor air bleed valve control apparatus
US3971208A (en) * 1974-04-01 1976-07-27 The Garrett Corporation Gas turbine fuel control
US3918254A (en) * 1974-05-16 1975-11-11 Woodward Governor Co Fuel control for a gas turbine having auxiliary air bleed

Also Published As

Publication number Publication date
JPS51146612A (en) 1976-12-16
CA1054385A (en) 1979-05-15
US4186556A (en) 1980-02-05
IT1060564B (it) 1982-08-20
FR2312657B1 (enExample) 1982-09-03
FR2312657A1 (fr) 1976-12-24
DE2623945C2 (de) 1986-04-17
DE2623945A1 (de) 1976-12-09
JPS5941012B2 (ja) 1984-10-04

Similar Documents

Publication Publication Date Title
JPS5236210A (en) Fuel system for gas turbine engine
IL51008A (en) Clearance control for gas turbine engine
GB1553847A (en) Fuel supply system for a gas turbine engine
GB1546722A (en) Gas turbine engine
IL53837A (en) Control system for gas turbine engine
GB1544454A (en) Gas turbine engines
GB1551860A (en) Gas turbine engines
GB1503457A (en) Gas turbine engines
JPS5236211A (en) Gas turbine engine
JPS51151410A (en) Fuel supply system for gas turbine engine
JPS523911A (en) Geometric control gas turbine engine
JPS5211314A (en) Gas turbine engine
GB2019494B (en) Gas turbine engine fuel system
GB2035461B (en) Fuel control for gas turbine engines
JPS5289717A (en) Fuel injector for gas turbine engine
JPS5214122A (en) Gas turbine engine
GB1555736A (en) Fuel system for gas turbine engieens
GB2045471B (en) Gas turbine engine fuel control systems
GB1549718A (en) Gas turbine engine
JPS5254826A (en) Cowling structure for gas turbine engine
IL60795A (en) Gas turbine fuel control system
GB1548713A (en) Gas turbine engine fuel control system
GB1550426A (en) Control system for gas turbine engines
GB1547770A (en) Gas turbine engine fuel injectocorsvk
GB1544826A (en) Turbofan gas turbine engines

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19920524