FR2882097B1 - Commande des geometries variables d'un moteur d'avion a turbine a gaz - Google Patents

Commande des geometries variables d'un moteur d'avion a turbine a gaz

Info

Publication number
FR2882097B1
FR2882097B1 FR0501639A FR0501639A FR2882097B1 FR 2882097 B1 FR2882097 B1 FR 2882097B1 FR 0501639 A FR0501639 A FR 0501639A FR 0501639 A FR0501639 A FR 0501639A FR 2882097 B1 FR2882097 B1 FR 2882097B1
Authority
FR
France
Prior art keywords
gas turbine
aircraft engine
controlling variable
turbine aircraft
variable geometries
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.)
Active
Application number
FR0501639A
Other languages
English (en)
Other versions
FR2882097A1 (fr
Inventor
Jean Marie Brocart
Regis Deldalle
Philippe Galozio
Michel Martini
Alain Michel Varizat
Maurice Vernochet
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.)
Safran Aircraft Engines SAS
Original Assignee
Hispano Suiza SA
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 Hispano Suiza SA filed Critical Hispano Suiza SA
Priority to FR0501639A priority Critical patent/FR2882097B1/fr
Priority to PCT/EP2006/060079 priority patent/WO2006087383A1/fr
Publication of FR2882097A1 publication Critical patent/FR2882097A1/fr
Application granted granted Critical
Publication of FR2882097B1 publication Critical patent/FR2882097B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/20—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
    • F01D17/22—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical
    • F01D17/24—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted the operation or power assistance being predominantly non-mechanical electrical
    • 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
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • 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
    • F05D2270/60—Control system actuates means
    • F05D2270/62—Electrical actuators

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Control Of Turbines (AREA)
FR0501639A 2005-02-17 2005-02-17 Commande des geometries variables d'un moteur d'avion a turbine a gaz Active FR2882097B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0501639A FR2882097B1 (fr) 2005-02-17 2005-02-17 Commande des geometries variables d'un moteur d'avion a turbine a gaz
PCT/EP2006/060079 WO2006087383A1 (fr) 2005-02-17 2006-02-17 Commande des geometries variables d'un moteur d'avion a turbine a gaz

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0501639A FR2882097B1 (fr) 2005-02-17 2005-02-17 Commande des geometries variables d'un moteur d'avion a turbine a gaz

Publications (2)

Publication Number Publication Date
FR2882097A1 FR2882097A1 (fr) 2006-08-18
FR2882097B1 true FR2882097B1 (fr) 2010-08-27

Family

ID=35124531

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0501639A Active FR2882097B1 (fr) 2005-02-17 2005-02-17 Commande des geometries variables d'un moteur d'avion a turbine a gaz

Country Status (2)

Country Link
FR (1) FR2882097B1 (fr)
WO (1) WO2006087383A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2531204C2 (ru) * 2009-04-16 2014-10-20 Эрсель Система управления для гондолы турбореактивного двигателя и гондола, оснащенная такой системой

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2911847B1 (fr) * 2007-01-31 2009-10-23 Hispano Suiza Sa Circuit d'alimentation en energie electrique pour des equipements electriques d'un moteur d'aeronef
FR2912782B1 (fr) * 2007-02-19 2009-05-22 Snecma Sa Procede de prelevement d'energie auxiliaire sur un turboreacteur d'avion et turboreacteur equipe pour mettre en oeuvre un tel procede
FR2940245B1 (fr) * 2008-12-22 2011-03-18 Messier Bugatti Architecture de distribution de puissance pour distribuer la puissance a des actionneurs electromecaniques d'un aeronef
FR2944563B1 (fr) 2009-04-16 2011-04-22 Aircelle Sa Dispositif d'inversion de poussee
US20130146708A1 (en) 2011-12-08 2013-06-13 Honeywell International Inc. Case assemblies with common controls
US20130145743A1 (en) 2011-12-08 2013-06-13 Honeywell International Inc. Case assembly with fuel driven actuation systems
EP2971593B1 (fr) 2013-03-13 2019-07-03 Rolls-Royce North American Technologies, Inc. Turbine à gaz et système électrique comprenant des bus électriques
US9488130B2 (en) 2013-10-17 2016-11-08 Honeywell International Inc. Variable area fan nozzle systems with improved drive couplings
CN113517785A (zh) * 2021-07-08 2021-10-19 中国航发湖南动力机械研究所 一种航空发动机交流发电机装置

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB939716A (en) * 1961-09-21 1963-10-16 Ass Elect Ind Improvements relating to automatic control equipment
GB1438767A (en) * 1972-10-03 1976-06-09 Lucas Industries Ltd Actuator device for use in a gas turbine engine
GB1405666A (en) * 1972-10-05 1975-09-10 Bergmann Borsig Veb Electric control system for steam or gas turbines
US4927329A (en) * 1988-10-21 1990-05-22 General Electric Company Aircraft engine unducted fan blade pitch control system
JPH05199704A (ja) * 1991-08-08 1993-08-06 General Electric Co <Ge> 電気アクチュエータ・モータ
DE4446621A1 (de) * 1994-12-24 1996-06-27 Klein Schanzlin & Becker Ag Frequenzgeregelter Stellmotor
US6129511A (en) * 1998-10-27 2000-10-10 Carrier Corporation Method and apparatus for controlling interaction between variable guide vanes and variable diffuser of a centrifugal compressor
GB9926354D0 (en) * 1999-11-08 2000-01-12 Rolls Royce Plc Power supply system for an aircraft
GB0116675D0 (en) * 2001-07-07 2001-08-29 Lucas Industries Ltd Vane actuator
US6789000B1 (en) * 2002-04-16 2004-09-07 Altek Power Corporation Microprocessor-based control system for gas turbine electric powerplant
FR2846377B1 (fr) * 2002-10-25 2006-06-30 Hispano Suiza Sa Inverseur de poussee electromecanique pour turboreacteur a controle permanent de position
US6778414B2 (en) * 2002-12-20 2004-08-17 The Boeing Company Distributed system and methodology of electrical power regulation, conditioning and distribution on an aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2531204C2 (ru) * 2009-04-16 2014-10-20 Эрсель Система управления для гондолы турбореактивного двигателя и гондола, оснащенная такой системой

Also Published As

Publication number Publication date
FR2882097A1 (fr) 2006-08-18
WO2006087383A1 (fr) 2006-08-24

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