FR2933144B1 - Nacelle pour aeronef comportant des moyens inverseurs de poussee et aeronef comportant au moins une telle nacelle - Google Patents

Nacelle pour aeronef comportant des moyens inverseurs de poussee et aeronef comportant au moins une telle nacelle

Info

Publication number
FR2933144B1
FR2933144B1 FR0854270A FR0854270A FR2933144B1 FR 2933144 B1 FR2933144 B1 FR 2933144B1 FR 0854270 A FR0854270 A FR 0854270A FR 0854270 A FR0854270 A FR 0854270A FR 2933144 B1 FR2933144 B1 FR 2933144B1
Authority
FR
France
Prior art keywords
nacelle
aircraft
inverter
pushing means
pushing
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
FR0854270A
Other languages
English (en)
Other versions
FR2933144A1 (fr
Inventor
Robert Andre
Benoit Letay
Benjamin Saget
Eric Inghelbrecht
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 FR0854270A priority Critical patent/FR2933144B1/fr
Priority to US12/491,746 priority patent/US8109468B2/en
Publication of FR2933144A1 publication Critical patent/FR2933144A1/fr
Application granted granted Critical
Publication of FR2933144B1 publication Critical patent/FR2933144B1/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
    • F02K1/64—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
    • 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • 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)
  • Wind Motors (AREA)
FR0854270A 2008-06-26 2008-06-26 Nacelle pour aeronef comportant des moyens inverseurs de poussee et aeronef comportant au moins une telle nacelle Active FR2933144B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0854270A FR2933144B1 (fr) 2008-06-26 2008-06-26 Nacelle pour aeronef comportant des moyens inverseurs de poussee et aeronef comportant au moins une telle nacelle
US12/491,746 US8109468B2 (en) 2008-06-26 2009-06-25 Nacelle for aircraft comprising means of reversing thrust and aircraft comprising at least one such nacelle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0854270A FR2933144B1 (fr) 2008-06-26 2008-06-26 Nacelle pour aeronef comportant des moyens inverseurs de poussee et aeronef comportant au moins une telle nacelle

Publications (2)

Publication Number Publication Date
FR2933144A1 FR2933144A1 (fr) 2010-01-01
FR2933144B1 true FR2933144B1 (fr) 2012-08-17

Family

ID=40325760

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0854270A Active FR2933144B1 (fr) 2008-06-26 2008-06-26 Nacelle pour aeronef comportant des moyens inverseurs de poussee et aeronef comportant au moins une telle nacelle

Country Status (2)

Country Link
US (1) US8109468B2 (fr)
FR (1) FR2933144B1 (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0606982D0 (en) * 2006-04-07 2006-05-17 Rolls Royce Plc Aeroengine thrust reverser
RU2494272C1 (ru) * 2012-04-02 2013-09-27 Открытое акционерное общество "Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева" (ОАО "ТАНТК им. Г.М. Бериева") Устройство реверса-нейтрализатора тяги двухконтурного турбореактивного двигателя самолета-амфибии
US8904751B2 (en) * 2012-04-30 2014-12-09 Middle River Aircraft Systems Thrust reverser assembly and method of operation
US9938929B2 (en) * 2014-03-21 2018-04-10 Rohr, Inc. Thrust reverser for a turbofan engine
US9739235B2 (en) * 2014-03-21 2017-08-22 Rohr, Inc. Thrust reverser for a turbofan engine
US10077739B2 (en) * 2014-04-24 2018-09-18 Rohr, Inc. Dual actuation system for cascade and thrust reverser panel for an integral cascade variable area fan nozzle
US9784214B2 (en) 2014-11-06 2017-10-10 Rohr, Inc. Thrust reverser with hidden linkage blocker doors
US10309343B2 (en) 2014-11-06 2019-06-04 Rohr, Inc. Split sleeve hidden door thrust reverser
US10605197B2 (en) * 2014-12-02 2020-03-31 United Technologies Corporation Gas turbine engine and thrust reverser assembly therefore
US10533519B2 (en) 2016-01-13 2020-01-14 Rohr, Inc. Translating cascade hidden blocker door thrust reverser
US10655564B2 (en) 2016-05-13 2020-05-19 Rohr, Inc. Thrust reverser system with hidden blocker doors
US9976696B2 (en) 2016-06-21 2018-05-22 Rohr, Inc. Linear actuator with multi-degree of freedom mounting structure
FR3055669B1 (fr) * 2016-09-05 2018-09-28 Airbus Operations Systeme d'inverseur de poussee limitant les perturbations aerodynamiques en configuration inactive
FR3057618A1 (fr) 2016-10-17 2018-04-20 Airbus Nacelle d'un turboreacteur comportant un volet inverseur
GB2564891A (en) 2017-07-26 2019-01-30 Short Brothers Plc Nacelle with thrust reverser
FR3074852B1 (fr) * 2017-12-13 2021-01-01 Airbus Operations Sas Nacelle d'un turboreacteur comportant un volet inverseur et une grille de deviation pour la formation d'un flux d'inversion
US10995701B2 (en) * 2019-09-05 2021-05-04 Rohr, Inc. Translating sleeve thrust reverser assembly
FR3115836B1 (fr) 2020-11-03 2022-10-21 Airbus Operations Sas Turboreacteur double flux comportant une serie de lames rotatives pour obturer la veine du flux secondaire

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3036431A (en) * 1959-09-08 1962-05-29 Boeing Co Thrust reverser for jet engines
GB1211923A (en) * 1968-08-30 1970-11-11 Rolls Royce Thrust reverser for gas turbine jet propulsion engine
GB1276265A (en) * 1970-04-15 1972-06-01 Rolls Royce Improvements in or relating to thrust deflectors for gas turbine ducted fan engines
US3665709A (en) * 1970-06-04 1972-05-30 Rohr Corp Thrust reversing apparatus
DE3280226D1 (de) * 1982-09-29 1990-09-13 Boeing Co Tuervorrichtung fuer schubumkehrblockierung.
FR2764341B1 (fr) * 1997-06-05 1999-07-16 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes formant ecopes associees a un deflecteur mobile
FR2887225B1 (fr) 2005-06-21 2008-09-19 Airbus France Sas Nacelle d'aeronef, et aeronef muni d'au moins une telle nacelle
GB0606982D0 (en) * 2006-04-07 2006-05-17 Rolls Royce Plc Aeroengine thrust reverser
FR2916737B1 (fr) * 2007-06-01 2010-05-28 Airbus France Ensemble moteur pour aeronef a nacelle coulissante.

Also Published As

Publication number Publication date
US20090321561A1 (en) 2009-12-31
US8109468B2 (en) 2012-02-07
FR2933144A1 (fr) 2010-01-01

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