FR2947868B1 - Nacelle d'aeronef incorporant un dispositif pour inverser la poussee - Google Patents

Nacelle d'aeronef incorporant un dispositif pour inverser la poussee

Info

Publication number
FR2947868B1
FR2947868B1 FR0954735A FR0954735A FR2947868B1 FR 2947868 B1 FR2947868 B1 FR 2947868B1 FR 0954735 A FR0954735 A FR 0954735A FR 0954735 A FR0954735 A FR 0954735A FR 2947868 B1 FR2947868 B1 FR 2947868B1
Authority
FR
France
Prior art keywords
reverting
push
aircraft nacelle
nacelle incorporating
incorporating
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 - Fee Related
Application number
FR0954735A
Other languages
English (en)
Other versions
FR2947868A1 (fr
Inventor
Benoit Letay
Benjamin Saget
Franck Lesieur
Stephane Flin
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 Operations SAS
Original Assignee
Airbus Operations 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 Operations SAS filed Critical Airbus Operations SAS
Priority to FR0954735A priority Critical patent/FR2947868B1/fr
Priority to US12/825,393 priority patent/US8701386B2/en
Publication of FR2947868A1 publication Critical patent/FR2947868A1/fr
Application granted granted Critical
Publication of FR2947868B1 publication Critical patent/FR2947868B1/fr
Expired - Fee Related 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
    • F02K1/64—Reversing fan flow
    • F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
    • F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
    • 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
    • F02K1/64—Reversing fan flow
    • F02K1/68—Reversers mounted on the engine housing downstream of the fan exhaust section
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/14—Casings or housings protecting or supporting assemblies within

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)
FR0954735A 2009-07-08 2009-07-08 Nacelle d'aeronef incorporant un dispositif pour inverser la poussee Expired - Fee Related FR2947868B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0954735A FR2947868B1 (fr) 2009-07-08 2009-07-08 Nacelle d'aeronef incorporant un dispositif pour inverser la poussee
US12/825,393 US8701386B2 (en) 2009-07-08 2010-06-29 Aircraft nacelle that incorporates a thrust reversal device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0954735A FR2947868B1 (fr) 2009-07-08 2009-07-08 Nacelle d'aeronef incorporant un dispositif pour inverser la poussee

Publications (2)

Publication Number Publication Date
FR2947868A1 FR2947868A1 (fr) 2011-01-14
FR2947868B1 true FR2947868B1 (fr) 2011-12-16

Family

ID=41612375

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0954735A Expired - Fee Related FR2947868B1 (fr) 2009-07-08 2009-07-08 Nacelle d'aeronef incorporant un dispositif pour inverser la poussee

Country Status (2)

Country Link
US (1) US8701386B2 (fr)
FR (1) FR2947868B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2947868B1 (fr) * 2009-07-08 2011-12-16 Airbus Operations Sas Nacelle d'aeronef incorporant un dispositif pour inverser la poussee
WO2014092757A1 (fr) * 2012-12-11 2014-06-19 United Technologies Corporation Inverseurs de poussée asymétriques
EP2971657B1 (fr) * 2013-03-12 2021-08-04 Raytheon Technologies Corporation Dispositif de commande d'écoulement à coque expansible
US9574519B2 (en) * 2013-08-23 2017-02-21 Rohr, Inc. Multi surface blocker door system and apparatus
EP2982854B1 (fr) * 2014-08-08 2023-03-01 Raytheon Technologies Corporation Buse de sortie divergente convergente pour un moteur à turbine à gaz
US11905913B2 (en) * 2021-10-22 2024-02-20 Spirit Aerosystems, Inc. Thrust reverser interspatial blocker system

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3303653A (en) * 1965-06-30 1967-02-14 Gen Electric Lightweight thrust reverser
GB1127828A (en) * 1966-06-29 1968-09-18 Rolls Royce Fan thrust reverser for jet propulsion plant
US3598318A (en) * 1970-04-10 1971-08-10 Boeing Co Movable acoustic splitter for nozzle area control and thrust reversal
US3815357A (en) * 1971-01-28 1974-06-11 Rohr Industries Inc Thrust reversing apparatus
GB1424193A (en) * 1972-03-21 1976-02-11 Rolls Royce Gas turbine ducted fan engines
US3831376A (en) * 1973-02-05 1974-08-27 Boeing Co Thrust reverser
US4073440A (en) * 1976-04-29 1978-02-14 The Boeing Company Combination primary and fan air thrust reversal control systems for long duct fan jet engines
US5699966A (en) * 1980-03-31 1997-12-23 General Electric Company Exhaust nozzle of a gas turbine engine
WO1983003281A1 (fr) * 1982-03-17 1983-09-29 Klees, Garry, William Attenuateur de bruit ventile interieurement avec diffuseur a large tampon
WO2008045091A1 (fr) * 2006-10-12 2008-04-17 United Technologies Corporation Buse à section variable d'un ventilateur de turbine à gaz équipée d'un système à pièces rapportées pivotantes
US7681399B2 (en) * 2006-11-14 2010-03-23 General Electric Company Turbofan engine cowl assembly and method of operating the same
FR2947868B1 (fr) * 2009-07-08 2011-12-16 Airbus Operations Sas Nacelle d'aeronef incorporant un dispositif pour inverser la poussee

Also Published As

Publication number Publication date
FR2947868A1 (fr) 2011-01-14
US8701386B2 (en) 2014-04-22
US20110127353A1 (en) 2011-06-02

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