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FR2959532B1 - Nacelle de turboreacteur - Google Patents

Nacelle de turboreacteur

Info

Publication number
FR2959532B1
FR2959532B1 FR1053373A FR1053373A FR2959532B1 FR 2959532 B1 FR2959532 B1 FR 2959532B1 FR 1053373 A FR1053373 A FR 1053373A FR 1053373 A FR1053373 A FR 1053373A FR 2959532 B1 FR2959532 B1 FR 2959532B1
Authority
FR
France
Prior art keywords
turboreactor
nacelle
turboreactor nacelle
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
FR1053373A
Other languages
English (en)
Other versions
FR2959532A1 (fr
Inventor
Pierre Caruel
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 Nacelles SAS
Original Assignee
Aircelle 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
Priority to FR1053373A priority Critical patent/FR2959532B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to CN201180021748.4A priority patent/CN102859168B/zh
Priority to BR112012026719A priority patent/BR112012026719A2/pt
Priority to PCT/FR2011/050924 priority patent/WO2011135238A1/fr
Priority to EP11731443A priority patent/EP2564050A1/fr
Priority to CA2796743A priority patent/CA2796743A1/fr
Priority to RU2012149588/06A priority patent/RU2012149588A/ru
Publication of FR2959532A1 publication Critical patent/FR2959532A1/fr
Priority to US13/663,652 priority patent/US20130228635A1/en
Application granted granted Critical
Publication of FR2959532B1 publication Critical patent/FR2959532B1/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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/09—Varying effective area of jet pipe or nozzle by axially moving an external member, e.g. a shroud

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Steering Controls (AREA)
  • Control Of Turbines (AREA)
FR1053373A 2010-04-30 2010-04-30 Nacelle de turboreacteur Expired - Fee Related FR2959532B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1053373A FR2959532B1 (fr) 2010-04-30 2010-04-30 Nacelle de turboreacteur
BR112012026719A BR112012026719A2 (pt) 2010-04-30 2011-04-21 nacela de motor turbojato de desvio equipada com um dispositivo reversor de empuxo compreendendo uma capota e meios de desvio suportados por uma moldura frontal a montante da capota e método de variação de uma seção transversal de um bocal de tubo de jato de uma nacela implementado com a nacela.
PCT/FR2011/050924 WO2011135238A1 (fr) 2010-04-30 2011-04-21 Nacelle de turboréacteur
EP11731443A EP2564050A1 (fr) 2010-04-30 2011-04-21 Nacelle de turboréacteur
CN201180021748.4A CN102859168B (zh) 2010-04-30 2011-04-21 涡轮喷气发动机舱
CA2796743A CA2796743A1 (fr) 2010-04-30 2011-04-21 Nacelle de turboreacteur
RU2012149588/06A RU2012149588A (ru) 2010-04-30 2011-04-21 Гондола турбореактивного двигателя
US13/663,652 US20130228635A1 (en) 2010-04-30 2012-10-30 Turbojet engine nacelle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1053373A FR2959532B1 (fr) 2010-04-30 2010-04-30 Nacelle de turboreacteur

Publications (2)

Publication Number Publication Date
FR2959532A1 FR2959532A1 (fr) 2011-11-04
FR2959532B1 true FR2959532B1 (fr) 2013-01-04

Family

ID=43143712

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1053373A Expired - Fee Related FR2959532B1 (fr) 2010-04-30 2010-04-30 Nacelle de turboreacteur

Country Status (8)

Country Link
US (1) US20130228635A1 (fr)
EP (1) EP2564050A1 (fr)
CN (1) CN102859168B (fr)
BR (1) BR112012026719A2 (fr)
CA (1) CA2796743A1 (fr)
FR (1) FR2959532B1 (fr)
RU (1) RU2012149588A (fr)
WO (1) WO2011135238A1 (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2957979B1 (fr) * 2010-03-25 2012-03-30 Aircelle Sa Dispositif d'inversion de poussee
FR2991670B1 (fr) * 2012-06-12 2014-06-20 Aircelle Sa Inverseur de poussee a grilles retractables et tuyere variable
FR3007800B1 (fr) * 2013-07-01 2017-10-20 Aircelle Sa Inverseur de poussee d’une nacelle de turboreacteur, comprenant des grilles partiellement integrees dans les capots
US9945324B2 (en) 2014-11-06 2018-04-17 Rohr, Inc. Sleeve linkage for thrust reverser
FR3065260B1 (fr) * 2017-04-14 2020-10-09 Safran Aircraft Engines Systeme inverseur de poussee pour turboreacteur
FR3067406B1 (fr) 2017-06-13 2019-07-12 Airbus Operations Systeme d'inverseur de poussee presentant des perturbations aerodynamiques limitees
US10436112B2 (en) * 2017-06-26 2019-10-08 The Boeing Company Translating turning vanes for a nacelle inlet
FR3078951B1 (fr) 2018-03-13 2020-02-28 Airbus Operations Turboreacteur comportant une nacelle equipee d'un carter de soufflante et d'une structure fixe

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1276265A (en) * 1970-04-15 1972-06-01 Rolls Royce Improvements in or relating to thrust deflectors for gas turbine ducted fan engines
US3658253A (en) * 1970-07-01 1972-04-25 Fred W Steffen Thrust reverser for plug type jet engine nozzle
GB1386232A (en) * 1971-03-31 1975-03-05 Short Brothers & Harland Ltd Fluid propulsion systems
US3829020A (en) * 1973-06-13 1974-08-13 Boeing Co Translating sleeve variable area nozzle and thrust reverser
US4802629A (en) * 1982-10-22 1989-02-07 The Boeing Company Plug-type exhaust nozzle having a variable centerbody and translating shroud
GB2189550A (en) * 1986-04-25 1987-10-28 Rolls Royce A gas turbine engine powerplant with flow control devices
FR2622929A1 (fr) * 1987-11-05 1989-05-12 Hispano Suiza Sa Inverseur de poussee de turboreacteur a grilles,a section variable d'ejection
US5778659A (en) * 1994-10-20 1998-07-14 United Technologies Corporation Variable area fan exhaust nozzle having mechanically separate sleeve and thrust reverser actuation systems
US5806302A (en) * 1996-09-24 1998-09-15 Rohr, Inc. Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser
GB0606982D0 (en) * 2006-04-07 2006-05-17 Rolls Royce Plc Aeroengine thrust reverser
FR2902839B1 (fr) * 2006-06-21 2011-09-30 Aircelle Sa Inverseur de poussee formant une tuyere adaptative
FR2914700B1 (fr) * 2007-04-04 2009-05-22 Aircelle Sa Inverseur de poussee pour moteur a reaction

Also Published As

Publication number Publication date
US20130228635A1 (en) 2013-09-05
WO2011135238A1 (fr) 2011-11-03
CA2796743A1 (fr) 2011-11-03
FR2959532A1 (fr) 2011-11-04
RU2012149588A (ru) 2014-06-20
BR112012026719A2 (pt) 2016-07-12
CN102859168B (zh) 2015-12-16
EP2564050A1 (fr) 2013-03-06
CN102859168A (zh) 2013-01-02

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Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 6

ST Notification of lapse

Effective date: 20161230