GB1498664A - Gas turbine fuel control - Google Patents

Gas turbine fuel control

Info

Publication number
GB1498664A
GB1498664A GB12949/75A GB1294975A GB1498664A GB 1498664 A GB1498664 A GB 1498664A GB 12949/75 A GB12949/75 A GB 12949/75A GB 1294975 A GB1294975 A GB 1294975A GB 1498664 A GB1498664 A GB 1498664A
Authority
GB
United Kingdom
Prior art keywords
surge
schedule
engine
fuel
fuel flow
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
GB12949/75A
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.)
Garrett Corp
Original Assignee
Garrett 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 Garrett Corp filed Critical Garrett Corp
Publication of GB1498664A publication Critical patent/GB1498664A/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)
GB12949/75A 1974-04-01 1975-03-27 Gas turbine fuel control Expired GB1498664A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/456,492 US3971208A (en) 1974-04-01 1974-04-01 Gas turbine fuel control

Publications (1)

Publication Number Publication Date
GB1498664A true GB1498664A (en) 1978-01-25

Family

ID=23812981

Family Applications (1)

Application Number Title Priority Date Filing Date
GB12949/75A Expired GB1498664A (en) 1974-04-01 1975-03-27 Gas turbine fuel control

Country Status (3)

Country Link
US (1) US3971208A (enExample)
FR (1) FR2265990B1 (enExample)
GB (1) GB1498664A (enExample)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2128771A (en) * 1982-10-13 1984-05-02 Rolls Royce Fuel control system for a gas turbine engine
GB2134285A (en) * 1983-01-28 1984-08-08 Gen Electric Control of gas turbines
CN112412632A (zh) * 2020-11-19 2021-02-26 中国航发沈阳发动机研究所 一种基于进口流量匹配的航空发动机喘振切油方法及系统

Families Citing this family (50)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4134258A (en) * 1974-06-10 1979-01-16 Nippondenso Co., Ltd. Fuel control system
US4186556A (en) * 1975-05-29 1980-02-05 General Electric Company Compressor bleed biased acceleration schedule
US4155684A (en) * 1975-10-17 1979-05-22 Bbc Brown Boveri & Company Limited Two-stage exhaust-gas turbocharger
US4055946A (en) * 1976-03-29 1977-11-01 United Technologies Corporation Twin-spool gas turbine power plant with means to spill compressor interstage airflow
GB1591217A (en) * 1977-10-17 1981-06-17 Garrett Corp Engine fuel control system
US4249238A (en) * 1978-05-24 1981-02-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus for sensor failure detection and correction in a gas turbine engine control system
US4251987A (en) * 1979-08-22 1981-02-24 General Electric Company Differential geared engine
US4296601A (en) * 1979-08-23 1981-10-27 Otis Elevator Company Electronic fuel control system
FR2488696A1 (fr) * 1980-08-13 1982-02-19 Snecma Procede et dispositif de detection du decollement tournant apparaissant dans une turbomachine a deux corps tournants
US4470118A (en) * 1982-04-19 1984-09-04 Chandler Evans Inc. Gas turbine engine fuel control
US4490791A (en) * 1982-04-19 1984-12-25 Chandler Evans Inc. Adaptive gas turbine acceleration control
US4672806A (en) * 1983-01-28 1987-06-16 General Electric Company Isochronous gas turbine speed control
US4598544A (en) * 1983-04-28 1986-07-08 Williams International Corporation Medium bypass turbofan engine
US4502275A (en) * 1983-10-13 1985-03-05 Avco Corporation Compressor air bleed override control system
US4700542A (en) * 1984-09-21 1987-10-20 Wang Lin Shu Internal combustion engines and methods of operation
US4912642A (en) * 1987-09-03 1990-03-27 The Boeing Company Coordinated engine autothrottle
US5447023A (en) * 1992-06-30 1995-09-05 United Technologies Corporation Synthesized fuel flow rate and metering valve position
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
US6171055B1 (en) * 1998-04-03 2001-01-09 Aurora Flight Sciences Corporation Single lever power controller for manned and unmanned aircraft
US6557400B2 (en) * 2001-03-30 2003-05-06 Honeywell International Inc. Surge bleed valve fault detection
US6748744B2 (en) * 2001-11-21 2004-06-15 Pratt & Whitney Canada Corp. Method and apparatus for the engine control of output shaft speed
US6688097B2 (en) 2001-12-19 2004-02-10 Honeywell International Inc. Multivariant set point using N1 and N2 for engine control
US7121078B2 (en) * 2003-01-28 2006-10-17 General Electric Company Methods and apparatus for operating gas turbine engines
GB0307035D0 (en) * 2003-03-26 2003-04-30 Rolls Royce Plc Acceleration control in a multi-spool gas turbine engine
US7010904B2 (en) * 2003-12-05 2006-03-14 United Technologies Corporation Method for control scheduling to achieve linear thrust response
JP2005226584A (ja) * 2004-02-13 2005-08-25 Honda Motor Co Ltd コンプレッサ及びガスタービンエンジン
US7826954B2 (en) * 2004-06-25 2010-11-02 Honda Motor Co., Ltd. System for monitoring sensor outputs of a gas turbine engine
US7509810B2 (en) * 2004-11-10 2009-03-31 Honeywell International Inc. Inter-turbine temperature display compensation method
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
WO2006059982A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Remote engine fuel control and electronic engine control for turbine engine
US20070245710A1 (en) * 2006-04-21 2007-10-25 Honeywell International, Inc. Optimized configuration of a reverse flow combustion system for a gas turbine engine
US7762078B2 (en) * 2006-09-13 2010-07-27 Aerojet-General Corporation Nozzle with temperature-responsive throat diameter
US8601786B2 (en) * 2006-10-12 2013-12-10 United Technologies Corporation Operational line management of low pressure compressor in a turbofan engine
US10041407B2 (en) 2011-03-29 2018-08-07 General Electric Company System and method for air extraction from gas turbine engines
US8777793B2 (en) 2011-04-27 2014-07-15 United Technologies Corporation Fan drive planetary gear system integrated carrier and torque frame
US20130195645A1 (en) * 2012-01-31 2013-08-01 Gabriel L. Suciu Geared turbomachine architecture having a low profile core flow path contour
US8863491B2 (en) 2012-01-31 2014-10-21 United Technologies Corporation Gas turbine engine shaft bearing configuration
US10400629B2 (en) 2012-01-31 2019-09-03 United Technologies Corporation Gas turbine engine shaft bearing configuration
US9038366B2 (en) 2012-01-31 2015-05-26 United Technologies Corporation LPC flowpath shape with gas turbine engine shaft bearing configuration
US9200572B2 (en) 2012-09-13 2015-12-01 Pratt & Whitney Canada Corp. Compressor surge prevention digital system
EP3019728B1 (en) * 2013-07-12 2019-12-25 United Technologies Corporation Three spool geared turbofan with low pressure compressor drive gear system
US9982676B2 (en) * 2014-11-18 2018-05-29 Rolls-Royce North American Technologies Inc. Split axial-centrifugal compressor
US10329943B2 (en) 2014-11-18 2019-06-25 Rolls-Royce North American Technologies Inc. Split axial-centrifugal compressor
US10309249B2 (en) * 2015-04-17 2019-06-04 Honda Motor Co., Ltd. Control apparatus for a gas-turbine aeroengine
US10061298B2 (en) * 2016-04-27 2018-08-28 General Electric Company Control of machinery with calibrated performance model
US20180058462A1 (en) * 2016-08-23 2018-03-01 Honeywell International Inc. Gas turbine engine compressor surge avoidance control system and method
GB201900733D0 (en) * 2019-01-18 2019-03-06 Rolls Royce Plc Highly loaded inlet duct in a geared turbofan
EP3751117B1 (en) * 2019-06-12 2024-05-29 Rolls-Royce plc Increasing compression efficiency via shaft power transfer
CN112065592B (zh) * 2020-08-13 2021-12-28 中国航发沈阳发动机研究所 一种未充分暖机条件下避免发动机喘振的加速控制方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3006145A (en) * 1959-10-14 1961-10-31 Gen Motors Corp Antisurge control using compressor bleed
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
GB1215931A (en) * 1967-03-11 1970-12-16 Rolls Royce Improvements in or relating to gas turbine engines
US3646753A (en) * 1970-04-28 1972-03-07 United Aircraft Corp Engine compressor bleed control system
US3638422A (en) * 1970-06-26 1972-02-01 Gen Electric Two-shaft gas turbine control system
US3686860A (en) * 1970-09-25 1972-08-29 Chandler Evans Inc Nozzle control
US3710576A (en) * 1971-02-22 1973-01-16 D Evans Dual clutch free turbine engine
US3797233A (en) * 1973-06-28 1974-03-19 United Aircraft Corp Integrated control for a turbopropulsion system

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2128771A (en) * 1982-10-13 1984-05-02 Rolls Royce Fuel control system for a gas turbine engine
GB2134285A (en) * 1983-01-28 1984-08-08 Gen Electric Control of gas turbines
GB2180372A (en) * 1983-01-28 1987-03-25 Gen Electric Isochronous gas turbine speed control
CN112412632A (zh) * 2020-11-19 2021-02-26 中国航发沈阳发动机研究所 一种基于进口流量匹配的航空发动机喘振切油方法及系统
CN112412632B (zh) * 2020-11-19 2022-03-04 中国航发沈阳发动机研究所 一种基于进口流量匹配的航空发动机喘振切油方法及系统

Also Published As

Publication number Publication date
FR2265990B1 (enExample) 1977-07-08
US3971208A (en) 1976-07-27
FR2265990A1 (enExample) 1975-10-24

Similar Documents

Publication Publication Date Title
GB1498664A (en) Gas turbine fuel control
US4294069A (en) Exhaust nozzle control and core engine fuel control for turbofan engine
US6735955B2 (en) Control system for positioning compressor inlet guide vanes
US5133182A (en) Control of low compressor vanes and fuel for a gas turbine engine
US4157010A (en) Gas turbine engine with power modulation capability
US3523423A (en) Gas turbine engines
US3006145A (en) Antisurge control using compressor bleed
US4928482A (en) Control of high compressor vanes and fuel for a gas turbine engine
GB1313841A (en) Gas turbine jet propulsion engine
CA1086512A (en) Bleed valve control system
US4230439A (en) Air delivery system for regulating thermal growth
GB1179994A (en) Electronic Fuel Control System for Gas Turbine Engines.
US4984425A (en) Acceleration control for a gas turbine engine
US3888078A (en) Governing device for a gas turbine system exemplified by a vehicular or aircraft engine
US4186556A (en) Compressor bleed biased acceleration schedule
Roy-Aikins Considerations for the use of variable geometry in gas turbines
US3579992A (en) Power plant variable geometry control
US2960826A (en) Coordinated fuel and speed scheduling control for gas turbine engines
FR2083444B1 (enExample)
GB727201A (en) Improvements in fuel supply systems for gas turbine engines
GB1321333A (en) Gas turbine engines having variable pitch guide vanes
GB701324A (en) Improvements in jet or propeller turbine engines used for aircraft propulsion
GB837497A (en) Air intakes in aircraft engines
GB716811A (en) Improvements in gas turbines for the propulsion of vehicles, particularly locomotives
GB1084957A (en) Improvements in or relating to turbojets with afterburner and variable area nozzle means

Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PE20 Patent expired after termination of 20 years

Effective date: 19950326