FR2714423B1 - Mécanisme de commande d'inverseur de poussée. - Google Patents

Mécanisme de commande d'inverseur de poussée.

Info

Publication number
FR2714423B1
FR2714423B1 FR9415303A FR9415303A FR2714423B1 FR 2714423 B1 FR2714423 B1 FR 2714423B1 FR 9415303 A FR9415303 A FR 9415303A FR 9415303 A FR9415303 A FR 9415303A FR 2714423 B1 FR2714423 B1 FR 2714423B1
Authority
FR
France
Prior art keywords
control mechanism
thrust reverser
reverser control
thrust
reverser
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
FR9415303A
Other languages
English (en)
Other versions
FR2714423A1 (fr
Inventor
Arnold Charles Newton
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of FR2714423A1 publication Critical patent/FR2714423A1/fr
Application granted granted Critical
Publication of FR2714423B1 publication Critical patent/FR2714423B1/fr
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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Retarders (AREA)
FR9415303A 1993-12-24 1994-12-20 Mécanisme de commande d'inverseur de poussée. Expired - Lifetime FR2714423B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB939326466A GB9326466D0 (en) 1993-12-24 1993-12-24 Thrust reverser control mechanism

Publications (2)

Publication Number Publication Date
FR2714423A1 FR2714423A1 (fr) 1995-06-30
FR2714423B1 true FR2714423B1 (fr) 1997-07-18

Family

ID=10747238

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9415303A Expired - Lifetime FR2714423B1 (fr) 1993-12-24 1994-12-20 Mécanisme de commande d'inverseur de poussée.

Country Status (3)

Country Link
US (1) US5493856A (fr)
FR (1) FR2714423B1 (fr)
GB (2) GB9326466D0 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6311928B1 (en) 2000-01-05 2001-11-06 Stage Iii Technologies, L.C. Jet engine cascade thrust reverser for use with mixer/ejector noise suppressor
GB0608985D0 (en) * 2006-05-06 2006-06-14 Rolls Royce Plc Aeroengine thrust reverser
US9759087B2 (en) 2007-08-08 2017-09-12 Rohr, Inc. Translating variable area fan nozzle providing an upstream bypass flow exit
CN101939528B (zh) 2007-08-08 2013-07-24 罗尔股份有限公司 具有旁通流的面积可调风扇喷嘴
EP2278147B1 (fr) * 2009-06-16 2014-06-25 Rohr, Inc. Modulation de buse de ventilation à fente variable fournissant une sortie de dérivation d'écoulement en amont
US8875486B2 (en) 2010-05-17 2014-11-04 Rohr, Inc. Guide system for nacelle assembly
US8511973B2 (en) 2010-06-23 2013-08-20 Rohr, Inc. Guide system for nacelle assembly
CN113107701B (zh) * 2021-04-28 2022-02-22 中国航发沈阳发动机研究所 一种可调的喷管结构
US11933248B1 (en) * 2022-12-09 2024-03-19 Pratt & Whitney Canada Corp. Reverse thrust system and method

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3050937A (en) * 1958-06-09 1962-08-28 Boeing Co Reversible thrust jet engines and controls therefor
GB1450076A (en) * 1973-04-05 1976-09-22 Rolls Royce Control systems for gas rubine engines
FR2494775B1 (fr) * 1980-11-27 1985-07-05 Astech Dispositif pour la commande d'un inverseur de poussee pour moteur a reaction
GB9015373D0 (en) * 1990-07-12 1990-08-29 Rolls Royce Plc Gas turbine engine thrust reverser control
FR2679605A1 (fr) * 1991-07-24 1993-01-29 Snecma Inverseur de poussee de turboreacteur muni d'un dispositif de securite integre au systeme de commande hydraulique.
EP0536954B1 (fr) * 1991-10-10 1996-01-24 Lucas Industries Public Limited Company Dispositif de verrouillage d'un inverseur de poussée

Also Published As

Publication number Publication date
GB9424846D0 (en) 1995-02-08
GB2285020A (en) 1995-06-28
US5493856A (en) 1996-02-27
FR2714423A1 (fr) 1995-06-30
GB2285020B (en) 1997-10-22
GB9326466D0 (en) 1994-02-23

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