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BR8107625A - Sistema de controle de combustivel para motor de turbina a gas - Google Patents

Sistema de controle de combustivel para motor de turbina a gas

Info

Publication number
BR8107625A
BR8107625A BR8107625A BR8107625A BR8107625A BR 8107625 A BR8107625 A BR 8107625A BR 8107625 A BR8107625 A BR 8107625A BR 8107625 A BR8107625 A BR 8107625A BR 8107625 A BR8107625 A BR 8107625A
Authority
BR
Brazil
Prior art keywords
control system
gas turbine
turbine engine
fuel control
fuel
Prior art date
Application number
BR8107625A
Other languages
English (en)
Inventor
Rowland Marston Evans
Original Assignee
Aviat Electric 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 Aviat Electric Ltd filed Critical Aviat Electric Ltd
Publication of BR8107625A publication Critical patent/BR8107625A/pt

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
    • F05D2270/02—Purpose of the control system to control rotational speed (n)

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
BR8107625A 1980-11-28 1981-11-24 Sistema de controle de combustivel para motor de turbina a gas BR8107625A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/210,938 US4423592A (en) 1980-11-28 1980-11-28 Fuel control system for gas turbine engine

Publications (1)

Publication Number Publication Date
BR8107625A true BR8107625A (pt) 1982-08-24

Family

ID=22784945

Family Applications (1)

Application Number Title Priority Date Filing Date
BR8107625A BR8107625A (pt) 1980-11-28 1981-11-24 Sistema de controle de combustivel para motor de turbina a gas

Country Status (4)

Country Link
US (1) US4423592A (pt)
EP (1) EP0053547A1 (pt)
BR (1) BR8107625A (pt)
CA (1) CA1172730A (pt)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4593523A (en) * 1980-12-17 1986-06-10 Allied Corporation Method and apparatus for acceleration limiting a gas turbine engine
CA1177936A (en) * 1981-04-24 1984-11-13 Rowland M. Evans Stress limiter apparatus for a gas turbine engine
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
US4594852A (en) * 1984-10-30 1986-06-17 General Electric Company Aircraft engine control
US4993221A (en) * 1988-12-21 1991-02-19 General Electric Company Gas turbine engine control system
US5134845A (en) * 1990-07-23 1992-08-04 United Technologies Corporation Control for a gas turbine engine
US5361579A (en) * 1993-06-01 1994-11-08 Sundstrand Corporation Turbojet fuel control system
US5868763A (en) 1996-09-16 1999-02-09 Guidant Corporation Means and methods for performing an anastomosis
US6811555B1 (en) 1996-09-16 2004-11-02 Origin Medsystems, Inc. Method and apparatus for performing anastomosis with eversion of tissue edges and joining of exposed intima of the everted tissue
AU7341800A (en) * 1999-09-01 2001-03-26 Origin Medsystems, Inc. Method and apparatus for performing anastomosis
US6890338B1 (en) * 2001-02-27 2005-05-10 Origin Medsystems, Inc. Method and apparatus for performing anastomosis using ring having tines with weak sections
US7431015B2 (en) * 2006-01-31 2008-10-07 Honeywell International Inc. Fuel metering system proportional bypass valve error compensation system and method
US7712299B2 (en) * 2006-09-05 2010-05-11 Conocophillips Company Anti-bogdown control system for turbine/compressor systems
GB0620310D0 (en) * 2006-10-13 2006-11-22 Rolls Royce Plc Engine control
US8321119B2 (en) * 2008-07-10 2012-11-27 General Electric Company Methods and systems to facilitate over-speed protection
US20100005657A1 (en) * 2008-07-10 2010-01-14 Van Vactor David R Methods and systems to facilitate over-speed protection
US8224552B2 (en) * 2008-07-10 2012-07-17 General Electric Company Methods and systems to facilitate over-speed protection
FR2976622B1 (fr) * 2011-06-16 2015-05-01 Turbomeca Architecture double corps de turbomoteur avec compresseur haute pression lie a la turbine basse pression
US9382847B2 (en) * 2012-11-02 2016-07-05 Pratt & Whitney Canada Corp. Rotor resonance disturbance rejection controller
US9494085B2 (en) 2015-01-19 2016-11-15 United Technologies Corporation System and method for load power management in a turboshaft gas turbine engine
US9909442B2 (en) * 2015-07-02 2018-03-06 General Electric Company Method of controlling a position actuation system component for a gas turbine engine
US10584646B2 (en) * 2016-07-29 2020-03-10 Pratt & Whitney Canada Corp. System and method for control of gas turbine engine
CN115075954B (zh) * 2022-05-23 2023-03-28 蓝箭航天空间科技股份有限公司 提高发动机启动成功率的方法及装置
CN117170225B (zh) * 2023-10-09 2024-04-09 清华大学 基于转子加速度反馈的航空发动机增量式控制器
CN118705062B (zh) * 2024-08-29 2024-12-06 中国航发湖南动力机械研究所 航空涡轴发动机控制方法、装置、电子设备及存储介质

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3006144A (en) 1961-10-31 arnett etal
US3152444A (en) 1961-03-01 1964-10-13 Bendix Corp Fuel control apparatus for turbo-shaft engines
US3393691A (en) 1965-12-13 1968-07-23 Bendix Corp Fuel control having proportional plus integral governor with variable proportional and integral gains
US3587229A (en) 1969-03-17 1971-06-28 Bendix Corp Combustion engine fuel control having governor reset means
DE2162660C3 (de) 1971-12-17 1974-09-12 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Regeleinrichtung für eine Gasturbinenanlage, z.B. ein Kraftfahrzeug- oder Flugtriebwerk
US3832846A (en) 1972-04-27 1974-09-03 Woodward Governor Co Speed governor with fuel rate control
GB1470757A (en) * 1973-04-27 1977-04-21 Lucas Industries Ltd Fuel control systems for gas turbine engines
US3936226A (en) 1974-06-07 1976-02-03 United Technologies Corporation Control system for variable pitch fan propulsor with reverse pitch
GB1520412A (en) * 1974-07-09 1978-08-09 Lucas Industries Ltd Gas turbine engine fuel control systems
GB1519143A (en) * 1974-07-09 1978-07-26 Lucas Industries Ltd Electronic fuel control for a gas turbine engine
GB1520882A (en) * 1974-07-24 1978-08-09 Lucas Industries Ltd Electronic fuel control for a gas turbine engine
SE393160B (sv) 1975-08-29 1977-05-02 Stal Laval Turbin Ab Reglersystem med nodutlosningsanordning for gasturbinanleggning
US4134257A (en) 1976-11-03 1979-01-16 The Garrett Corporation Gas turbine fuel delivery and control system
GB1573095A (en) 1976-11-26 1980-08-13 Lucas Industries Ltd Fuel control for a multi engine gas turbine installation
DE2702774C3 (de) 1977-01-24 1980-12-18 Bodenseewerk Geraetetechnik Gmbh, 7770 Ueberlingen Vorrichtung zur Drehzahlregelung von Turbo-Luftstrahltriebwerken
US4188781A (en) 1978-04-25 1980-02-19 General Electric Company Non-linear dual mode regulator circuit

Also Published As

Publication number Publication date
US4423592A (en) 1984-01-03
EP0053547A1 (en) 1982-06-09
CA1172730A (en) 1984-08-14

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