FR2933126B1 - Actionnement d'un inverseur de poussee dans une turbomachine - Google Patents

Actionnement d'un inverseur de poussee dans une turbomachine

Info

Publication number
FR2933126B1
FR2933126B1 FR0803548A FR0803548A FR2933126B1 FR 2933126 B1 FR2933126 B1 FR 2933126B1 FR 0803548 A FR0803548 A FR 0803548A FR 0803548 A FR0803548 A FR 0803548A FR 2933126 B1 FR2933126 B1 FR 2933126B1
Authority
FR
France
Prior art keywords
turbomachine
actuating
thrust inverter
thrust
inverter
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
FR0803548A
Other languages
English (en)
Other versions
FR2933126A1 (fr
Inventor
Christophe Claude Philippe Nouhaud
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
SNECMA 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR0803548A priority Critical patent/FR2933126B1/fr
Priority to US12/489,830 priority patent/US8402743B2/en
Publication of FR2933126A1 publication Critical patent/FR2933126A1/fr
Application granted granted Critical
Publication of FR2933126B1 publication Critical patent/FR2933126B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • 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
    • F02C9/263—Control of fuel supply by means of fuel metering valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/766—Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Braking Arrangements (AREA)
  • Control Of Turbines (AREA)
FR0803548A 2008-06-25 2008-06-25 Actionnement d'un inverseur de poussee dans une turbomachine Active FR2933126B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0803548A FR2933126B1 (fr) 2008-06-25 2008-06-25 Actionnement d'un inverseur de poussee dans une turbomachine
US12/489,830 US8402743B2 (en) 2008-06-25 2009-06-23 Actuating of a thrust reverser in a turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0803548A FR2933126B1 (fr) 2008-06-25 2008-06-25 Actionnement d'un inverseur de poussee dans une turbomachine

Publications (2)

Publication Number Publication Date
FR2933126A1 FR2933126A1 (fr) 2010-01-01
FR2933126B1 true FR2933126B1 (fr) 2012-11-02

Family

ID=40380448

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0803548A Active FR2933126B1 (fr) 2008-06-25 2008-06-25 Actionnement d'un inverseur de poussee dans une turbomachine

Country Status (2)

Country Link
US (1) US8402743B2 (fr)
FR (1) FR2933126B1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2958060B1 (fr) * 2010-03-24 2012-04-27 Snecma Procede et dispositif de detection d'une defaillance electrique affectant un systeme electrique de commande d'un actionneur hydraulique de geometries variables d'un moteur d'aeronef.
US20130145743A1 (en) 2011-12-08 2013-06-13 Honeywell International Inc. Case assembly with fuel driven actuation systems
US20130146708A1 (en) * 2011-12-08 2013-06-13 Honeywell International Inc. Case assemblies with common controls
US9388778B2 (en) * 2013-07-19 2016-07-12 Woodward, Inc. Servo flow recirculation for an advanced thermal efficient aircraft engine fuel system
US9488130B2 (en) 2013-10-17 2016-11-08 Honeywell International Inc. Variable area fan nozzle systems with improved drive couplings
US9650993B2 (en) * 2013-10-23 2017-05-16 Honeywell International Inc. Rotary hydraulic motor driven hybrid thrust reverser actuation system with end-of-stroke snubbing
US9951717B2 (en) * 2015-04-15 2018-04-24 Hamilton Sundstrand Corporation Asymmetric load compensation system
FR3085184B1 (fr) * 2018-08-24 2020-08-14 Safran Nacelles Architecture de commande d'aeronef, d'au moins un actionneur d'un capot mobile de nacelle
US11597508B2 (en) 2021-05-13 2023-03-07 Beta Air, Llc Aircraft having reverse thrust capabilities

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3377799A (en) * 1966-01-03 1968-04-16 Gen Electric Mechanical integrators and control systems employing same
US3332234A (en) * 1966-03-24 1967-07-25 John P Lavash Fuel delivery systems
US3442218A (en) * 1966-04-12 1969-05-06 Gen Electric Dual purpose pump
US3696895A (en) * 1971-06-24 1972-10-10 Garrett Corp Fluidic control for motor and brake
FR2491126A1 (fr) * 1980-10-01 1982-04-02 Snecma Dispositif pour manoeuvrer les volets d'une tuyere de turbomachine
GB2116129A (en) * 1982-03-06 1983-09-21 Rolls Royce Anti-rotation lock
US4458582A (en) * 1982-10-18 1984-07-10 Sundstrand Corporation Automatic rigging arrangement for actuation systems
US6625973B1 (en) * 2001-02-23 2003-09-30 Lucas Industries Limited Lock mechanism
FR2821892B1 (fr) * 2001-03-08 2003-06-13 Hispano Suiza Sa Systeme d'actionnement du capotage mobile d'un inverseur de poussee dans un turboreacteur
US6598386B2 (en) * 2001-10-16 2003-07-29 Honeywell International, Inc. Jet engine thrust reverser system having torque limited synchronization
US6935097B2 (en) * 2003-04-17 2005-08-30 Honeywell International, Inc. Lock assembly that inhibits thrust reverser movement at or near the stowed position
US8015797B2 (en) * 2006-09-21 2011-09-13 Jean-Pierre Lair Thrust reverser nozzle for a turbofan gas turbine engine

Also Published As

Publication number Publication date
US8402743B2 (en) 2013-03-26
FR2933126A1 (fr) 2010-01-01
US20090320444A1 (en) 2009-12-31

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