DE69200584D1 - Einrichtung zur Drehzahlsteuerung eines Flugzeugtriebwerkes. - Google Patents

Einrichtung zur Drehzahlsteuerung eines Flugzeugtriebwerkes.

Info

Publication number
DE69200584D1
DE69200584D1 DE69200584T DE69200584T DE69200584D1 DE 69200584 D1 DE69200584 D1 DE 69200584D1 DE 69200584 T DE69200584 T DE 69200584T DE 69200584 T DE69200584 T DE 69200584T DE 69200584 D1 DE69200584 D1 DE 69200584D1
Authority
DE
Germany
Prior art keywords
speed control
aircraft engine
aircraft
engine
speed
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 - Lifetime
Application number
DE69200584T
Other languages
English (en)
Other versions
DE69200584T2 (de
Inventor
Bernard Bissey
Claude Maffre
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of DE69200584D1 publication Critical patent/DE69200584D1/de
Application granted granted Critical
Publication of DE69200584T2 publication Critical patent/DE69200584T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
DE69200584T 1991-08-12 1992-08-04 Einrichtung zur Drehzahlsteuerung eines Flugzeugtriebwerkes. Expired - Lifetime DE69200584T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9110237A FR2680386B1 (fr) 1991-08-12 1991-08-12 Dispositif pour la commande du regime des moteurs d'un aeronef.

Publications (2)

Publication Number Publication Date
DE69200584D1 true DE69200584D1 (de) 1994-12-01
DE69200584T2 DE69200584T2 (de) 1995-03-23

Family

ID=9416141

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69200584T Expired - Lifetime DE69200584T2 (de) 1991-08-12 1992-08-04 Einrichtung zur Drehzahlsteuerung eines Flugzeugtriebwerkes.

Country Status (4)

Country Link
US (1) US5277024A (de)
EP (1) EP0532374B1 (de)
DE (1) DE69200584T2 (de)
FR (1) FR2680386B1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1113160B1 (de) * 1999-12-28 2007-05-02 Techspace Aero Steuerungsvorrichtung für eine Maschine auf einem Prüfstand
US6886786B1 (en) * 2003-10-10 2005-05-03 The Boeing Company Engine thrust management—new design architecture
US8682562B2 (en) * 2009-05-08 2014-03-25 Rolls-Royce Corporation Turbine engine thrust scheduling
FR2950324B1 (fr) * 2009-09-23 2011-08-26 Eurocopter France Procede et dispositif d'aide au pilotage d'un aeronef en cas de pannes d'un indicateur de premiere limitation
FR2986866B1 (fr) * 2012-02-13 2014-02-21 Airbus Operations Sas Procede et dispositif d'affichage d'informations de vitesse sur un avion.
US9322341B2 (en) * 2013-03-12 2016-04-26 Pratt & Whitney Canada Corp. System and method for engine transient power response
US10801361B2 (en) 2016-09-09 2020-10-13 General Electric Company System and method for HPT disk over speed prevention
US20220194561A1 (en) * 2020-12-17 2022-06-23 The Boeing Company Systems and Methods for Overriding Autonomous Control of a Device
US11787527B2 (en) 2021-10-26 2023-10-17 Lockheed Martin Corporation Actuation system for cockpit control levers

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1026850A (en) * 1973-09-24 1978-02-21 Smiths Industries Limited Dual, simultaneously operating control system with fault detection
US4134257A (en) * 1976-11-03 1979-01-16 The Garrett Corporation Gas turbine fuel delivery and control system
US4248040A (en) * 1979-06-04 1981-02-03 General Electric Company Integrated control system for a gas turbine engine
US4407118A (en) * 1980-07-10 1983-10-04 Lucas Industries Limited Gas turbine engine fuel control system
GB2079988B (en) * 1980-07-10 1984-02-01 Lucas Industries Ltd Gas turbine engine fuel control system
GB2094405B (en) * 1980-08-21 1984-05-31 Garrett Corp Engine management system
US4478038A (en) * 1982-09-20 1984-10-23 Chandler Evans, Inc. Electronic fuel control with manual training mode
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
FR2580034B1 (de) * 1985-04-03 1987-05-29 Aerospatiale
GB2228977B (en) * 1985-08-02 1990-11-21 Lucas Ind Plc Running control for a gas turbine engine
US4821193A (en) * 1985-08-26 1989-04-11 General Electric Company Digital control for gas turbine engine
US4809500A (en) * 1987-02-03 1989-03-07 United Technologies Corporation Transient control system for gas turbine engine
US4794755A (en) * 1987-05-14 1989-01-03 The United States Of America As Represented By The Secretary Of The Air Force Back-up control system for F101 engine and its derivatives
GB2217477B (en) * 1988-04-05 1992-04-15 Rolls Royce Plc An engine control unit for a turbomachine
US5022224A (en) * 1989-05-30 1991-06-11 United Technologies Corporation Acceleration control with duct pressure loss compensation
US4984425A (en) * 1989-05-30 1991-01-15 United Technologies Corporation Acceleration control for a gas turbine engine
IL94506A (en) * 1989-05-30 1993-07-08 United Technologies Corp Acceleration control for a gas turbine engine with duct pressure loss compensation

Also Published As

Publication number Publication date
FR2680386B1 (fr) 1993-11-05
US5277024A (en) 1994-01-11
FR2680386A1 (fr) 1993-02-19
EP0532374B1 (de) 1994-10-26
DE69200584T2 (de) 1995-03-23
EP0532374A1 (de) 1993-03-17

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R071 Expiry of right

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