FR2929998B1 - Nacelle de turboreacteur a double flux - Google Patents

Nacelle de turboreacteur a double flux

Info

Publication number
FR2929998B1
FR2929998B1 FR0802036A FR0802036A FR2929998B1 FR 2929998 B1 FR2929998 B1 FR 2929998B1 FR 0802036 A FR0802036 A FR 0802036A FR 0802036 A FR0802036 A FR 0802036A FR 2929998 B1 FR2929998 B1 FR 2929998B1
Authority
FR
France
Prior art keywords
double flow
nacelle
flow turboreactor
turboreactor nacelle
double
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
FR0802036A
Other languages
English (en)
Other versions
FR2929998A1 (fr
Inventor
Guy Vauchel
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 FR0802036A priority Critical patent/FR2929998B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to CA2719155A priority patent/CA2719155A1/fr
Priority to BRPI0910935A priority patent/BRPI0910935A2/pt
Priority to CN2009801130527A priority patent/CN102007284A/zh
Priority to US12/937,462 priority patent/US20110030338A1/en
Priority to EP09742294A priority patent/EP2268910A2/fr
Priority to PCT/FR2009/050643 priority patent/WO2009136096A2/fr
Priority to RU2010145242/06A priority patent/RU2499904C2/ru
Publication of FR2929998A1 publication Critical patent/FR2929998A1/fr
Application granted granted Critical
Publication of FR2929998B1 publication Critical patent/FR2929998B1/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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1261—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a substantially axially movable structure
    • 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
    • F05D2260/50—Kinematic linkage, i.e. transmission of position
FR0802036A 2008-04-14 2008-04-14 Nacelle de turboreacteur a double flux Expired - Fee Related FR2929998B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR0802036A FR2929998B1 (fr) 2008-04-14 2008-04-14 Nacelle de turboreacteur a double flux
BRPI0910935A BRPI0910935A2 (pt) 2008-04-14 2009-04-09 desvio da nacela de motor turbojato e nacela
CN2009801130527A CN102007284A (zh) 2008-04-14 2009-04-09 旁通式涡轮喷气发动机机舱
US12/937,462 US20110030338A1 (en) 2008-04-14 2009-04-09 Bypass turbojet engine nacelle
CA2719155A CA2719155A1 (fr) 2008-04-14 2009-04-09 Nacelle de turboreacteur a double flux
EP09742294A EP2268910A2 (fr) 2008-04-14 2009-04-09 Nacelle de turboréacteur à double flux
PCT/FR2009/050643 WO2009136096A2 (fr) 2008-04-14 2009-04-09 Nacelle de turboréacteur à double flux
RU2010145242/06A RU2499904C2 (ru) 2008-04-14 2009-04-09 Гондола двухконтурного турбореактивного двигателя

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0802036A FR2929998B1 (fr) 2008-04-14 2008-04-14 Nacelle de turboreacteur a double flux

Publications (2)

Publication Number Publication Date
FR2929998A1 FR2929998A1 (fr) 2009-10-16
FR2929998B1 true FR2929998B1 (fr) 2011-08-12

Family

ID=40344725

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0802036A Expired - Fee Related FR2929998B1 (fr) 2008-04-14 2008-04-14 Nacelle de turboreacteur a double flux

Country Status (8)

Country Link
US (1) US20110030338A1 (fr)
EP (1) EP2268910A2 (fr)
CN (1) CN102007284A (fr)
BR (1) BRPI0910935A2 (fr)
CA (1) CA2719155A1 (fr)
FR (1) FR2929998B1 (fr)
RU (1) RU2499904C2 (fr)
WO (1) WO2009136096A2 (fr)

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FR2962977B1 (fr) 2010-07-20 2012-08-17 Airbus Operations Sas Nacelle pour aeronef
US8910482B2 (en) * 2011-02-02 2014-12-16 The Boeing Company Aircraft engine nozzle
FR2975971B1 (fr) * 2011-06-01 2013-05-17 Aircelle Sa Nacelle pour un turboreacteur double flux d'un aeronef
US9021813B2 (en) * 2011-07-18 2015-05-05 The Boeing Company Cable-actuated variable area fan nozzle with elastomeric seals
FR2978802B1 (fr) 2011-08-05 2017-07-14 Aircelle Sa Inverseur a grilles mobiles et tuyere variable par translation
US9151183B2 (en) * 2011-11-21 2015-10-06 United Technologies Corporation Retractable exhaust liner segment for gas turbine engines
FR2991670B1 (fr) 2012-06-12 2014-06-20 Aircelle Sa Inverseur de poussee a grilles retractables et tuyere variable
FR2993921B1 (fr) * 2012-07-26 2014-07-18 Snecma Procede pour ameliorer les performances du systeme d'ejection d'un turbomoteur d'aeronef a double flux separes, systeme d'ejection et turbomoteur correspondants.
US9765729B2 (en) * 2013-10-17 2017-09-19 Rohr, Inc. Thrust reverser fan ramp with blocker door pocket
US9863367B2 (en) 2013-11-01 2018-01-09 The Boeing Company Fan nozzle drive systems that lock thrust reversers
FR3021704B1 (fr) * 2014-05-30 2016-06-03 Aircelle Sa Nacelle pour turboreacteur d'aeronef comprenant une tuyere secondaire a portes rotatives
FR3022220B1 (fr) 2014-06-16 2016-05-27 Aircelle Sa Inverseur de poussee pour nacelle de turboreacteur d’aeronef
US9856742B2 (en) * 2015-03-13 2018-01-02 Rohr, Inc. Sealing system for variable area fan nozzle
FR3033841B1 (fr) 2015-03-17 2017-04-28 Aircelle Sa Inverseur de poussee pour nacelle de turboreacteur d’aeronef
FR3037108B1 (fr) 2015-06-02 2017-06-09 Aircelle Sa Inverseur de poussee pour nacelle de turboreacteur d'aeronef
CN106194494B (zh) * 2016-08-09 2018-01-05 南京理工大学 一种用于微型涡喷发动机加力燃烧室的可调喷管
FR3062637B1 (fr) 2017-02-07 2020-07-10 Airbus Operations (S.A.S.) Nacelle de turboreacteur comportant un mecanisme d'entrainement d'inverseur de poussee
FR3077606B1 (fr) * 2018-02-05 2020-01-17 Airbus Nacelle d'un turboreacteur comportant une porte exterieure d'inversion
FR3078999A1 (fr) * 2018-03-13 2019-09-20 Airbus Operations Turboreacteur double flux comportant une serie de lames rotatives pour obturer la veine du flux secondaire
FR3086007B1 (fr) 2018-09-18 2020-09-04 Safran Nacelles Nacelle de turboreacteur avec un inverseur de poussee a grilles comprenant un secteur de commande des volets
FR3090102A1 (fr) * 2018-12-17 2020-06-19 Airbus Operations Outil de mesure de pression comportant un fourreau pour sa mise en place dans une veine d’un moteur d’aeronef
CN112796882B (zh) * 2020-12-30 2022-03-15 长江大学 一种涡轮螺旋桨发动机反推***

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FR1164936A (fr) * 1957-01-21 1958-10-15 Bertin Et Cie Soc Silencieux pour conduits d'échappement et notamment pour tuyères de propulseurs àréaction
US2874538A (en) * 1957-03-22 1959-02-24 Marquardt Aircraft Company Thrust reverser for jet engine
FR1401425A (fr) * 1964-04-24 1965-06-04 Aviation Louis Breguet Sa Dispositif de tuyère d'éjection pour avions à réaction
FR1482538A (fr) * 1965-06-07 1967-05-26 Gen Electric Inverseur de poussée
US3262269A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
FR91242E (fr) * 1966-10-27 1968-05-03 Breguet Aviat Dispositif de tuyère d'éjection pour avions à réaction
US3568792A (en) * 1969-06-18 1971-03-09 Rohr Corp Sound-suppressing and thrust-reversing apparatus
GB1424193A (en) * 1972-03-21 1976-02-11 Rolls Royce Gas turbine ducted fan engines
GB1421153A (en) * 1972-03-25 1976-01-14 Rolls Royce Propulsion nozzle for ducted fan gas turbine jet propulsion engines
US3863867A (en) * 1973-12-26 1975-02-04 Boeing Co Thrust control apparatus for a jet propulsion engine and actuating mechanism therefor
GB2189550A (en) * 1986-04-25 1987-10-28 Rolls Royce A gas turbine engine powerplant with flow control devices
US4767055A (en) * 1987-03-27 1988-08-30 United Technologies Corporation Method and linkage for positioning a convergent flap and coaxial arc valve
US4978071A (en) * 1989-04-11 1990-12-18 General Electric Company Nozzle with thrust vectoring in the yaw direction
US5176340A (en) * 1991-11-26 1993-01-05 Lair Jean Pierre Thrust reverser with a planar exit opening
FR2730764B1 (fr) * 1995-02-21 1997-03-14 Hispano Suiza Sa Inverseur de poussee a portes associees a un panneau aval
US5806302A (en) * 1996-09-24 1998-09-15 Rohr, Inc. Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser
GB2347126B (en) * 1999-02-23 2003-02-12 Rolls Royce Plc Thrust reverser
GB2372729A (en) * 2001-03-03 2002-09-04 Rolls Royce Plc Thrust reverser arrangement with means for reducing noise
US6568172B2 (en) * 2001-09-27 2003-05-27 The Nordam Group, Inc. Converging nozzle thrust reverser
GB0124446D0 (en) * 2001-10-11 2001-12-05 Short Brothers Ltd Aircraft propulsive power unit
US6845607B2 (en) * 2002-01-09 2005-01-25 The Nordam Group, Inc. Variable area plug nozzle
US6966175B2 (en) * 2003-05-09 2005-11-22 The Nordam Group, Inc. Rotary adjustable exhaust nozzle
US7146796B2 (en) * 2003-09-05 2006-12-12 The Nordam Group, Inc. Nested latch thrust reverser
FR2860046B1 (fr) * 2003-09-19 2005-12-02 Snecma Moteurs Volet chaud commande de tuyere axisymetrique de turboreacteur
RU2315887C2 (ru) * 2005-12-23 2008-01-27 Открытое акционерное общество "Авиадвигатель" Турбореактивный двигатель сверхвысокой степени двухконтурности
US7624579B2 (en) * 2006-02-15 2009-12-01 United Technologies Corporation Convergent divergent nozzle with supported divergent seals
EP2074304B1 (fr) * 2006-10-12 2015-03-25 United Technologies Corporation Moteur à turbine à gaz avec tuyère de soufflante à trois corps à section variable et inverseur de poussée

Also Published As

Publication number Publication date
BRPI0910935A2 (pt) 2015-10-06
FR2929998A1 (fr) 2009-10-16
US20110030338A1 (en) 2011-02-10
WO2009136096A2 (fr) 2009-11-12
CN102007284A (zh) 2011-04-06
RU2499904C2 (ru) 2013-11-27
CA2719155A1 (fr) 2009-11-12
WO2009136096A3 (fr) 2010-01-07
EP2268910A2 (fr) 2011-01-05
RU2010145242A (ru) 2012-05-20

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ST Notification of lapse

Effective date: 20151231