BR112012008419A2 - dispositivo de reversão de empuxo de nacela de motor a jato - Google Patents

dispositivo de reversão de empuxo de nacela de motor a jato

Info

Publication number
BR112012008419A2
BR112012008419A2 BR112012008419A BR112012008419A BR112012008419A2 BR 112012008419 A2 BR112012008419 A2 BR 112012008419A2 BR 112012008419 A BR112012008419 A BR 112012008419A BR 112012008419 A BR112012008419 A BR 112012008419A BR 112012008419 A2 BR112012008419 A2 BR 112012008419A2
Authority
BR
Brazil
Prior art keywords
jet engine
engine nacelle
reversal device
thrust reversal
nacelle thrust
Prior art date
Application number
BR112012008419A
Other languages
English (en)
Inventor
Pierre Caruel
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
Application filed by Aircelle Sa filed Critical Aircelle Sa
Publication of BR112012008419A2 publication Critical patent/BR112012008419A2/pt

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
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • 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
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/314—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being inclined in relation to each other
    • 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

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)
  • Transmission Devices (AREA)
  • Superstructure Of Vehicle (AREA)
  • Body Structure For Vehicles (AREA)
BR112012008419A 2009-11-05 2010-10-22 dispositivo de reversão de empuxo de nacela de motor a jato BR112012008419A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0905294A FR2952128B1 (fr) 2009-11-05 2009-11-05 Dispositif d'inverseur de poussee
PCT/FR2010/052262 WO2011055056A1 (fr) 2009-11-05 2010-10-22 Dispositif d'inversion de poussee

Publications (1)

Publication Number Publication Date
BR112012008419A2 true BR112012008419A2 (pt) 2016-03-29

Family

ID=42245995

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012008419A BR112012008419A2 (pt) 2009-11-05 2010-10-22 dispositivo de reversão de empuxo de nacela de motor a jato

Country Status (8)

Country Link
US (1) US9074554B2 (pt)
EP (1) EP2496817A1 (pt)
CN (1) CN102597475B (pt)
BR (1) BR112012008419A2 (pt)
CA (1) CA2776262A1 (pt)
FR (1) FR2952128B1 (pt)
RU (1) RU2538348C2 (pt)
WO (1) WO2011055056A1 (pt)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2982323B1 (fr) 2011-11-07 2013-11-15 Aircelle Sa Dispositif d'inversion de poussee
FR2990474B1 (fr) 2012-05-10 2014-05-02 Aircelle Sa Inverseur de poussee a volet de blocage a deploiement controle
FR2994586B1 (fr) * 2012-08-20 2014-08-08 Aircelle Sa Ensemble de poussee a grilles pour turboreacteur d'aeronef
US9938929B2 (en) 2014-03-21 2018-04-10 Rohr, Inc. Thrust reverser for a turbofan engine
US9945324B2 (en) * 2014-11-06 2018-04-17 Rohr, Inc. Sleeve linkage for thrust reverser
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
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
FR3054266B1 (fr) * 2016-07-25 2018-08-31 Safran Nacelles Systeme d’actionnement d’un panneau de nacelle de turboreacteur
US10343786B2 (en) 2017-06-28 2019-07-09 General Electric Company System and method of operating a ducted fan propulsion system during aircraft taxi
US10119495B1 (en) 2017-06-28 2018-11-06 General Electric Company System and method of operating a ducted fan propulsion system inflight
FR3068395B1 (fr) * 2017-06-30 2020-09-11 Safran Nacelles Nacelle pour turboreacteur comportant un inverseur de poussee a grilles
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
FR3094412A1 (fr) * 2019-03-25 2020-10-02 Airbus Operations Turboreacteur double flux comportant une serie de lames rotatives pour obturer la veine du flux secondaire
FR3095013A1 (fr) * 2019-04-15 2020-10-16 Airbus Operations Turboreacteur double flux comportant une serie de lames rotatives pour obturer la veine du flux secondaire

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3262269A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
US3614037A (en) * 1969-09-22 1971-10-19 Boeing Co Aircraft combination thrust reverser and sound suppressor and a particular full range balanced thrust reverser
FR2133520A1 (pt) * 1971-04-16 1972-12-01 Aviat Supply R Uni
GB1388406A (en) * 1971-12-15 1975-03-26 Rolls Royce Gas turbine ducted fan engines
GB1583952A (en) * 1976-07-13 1981-02-04 Short Brothers & Harland Ltd Gas turbine engines
US4216926A (en) * 1978-06-30 1980-08-12 Rohr Industries, Inc. Linkage system for a turbo fan engine thrust reverser
US4313581A (en) * 1979-09-12 1982-02-02 Rohr Industries, Inc. Reverser door mechanisms
DE3008193C2 (de) 1980-03-04 1982-07-08 Dynamit Nobel Ag, 5210 Troisdorf Kältestabile, Katalytisch wirksame Lösung von Diisopropoxy-bis(2,4-pentandionato)-titan(IV)
US4767055A (en) * 1987-03-27 1988-08-30 United Technologies Corporation Method and linkage for positioning a convergent flap and coaxial arc valve
US4807434A (en) * 1987-12-21 1989-02-28 The Boeing Company Thrust reverser for high bypass jet engines
US5309711A (en) * 1991-08-21 1994-05-10 Rohr, Inc. Cascade type thrust reverser for fan jet engines
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
FR2745036B1 (fr) * 1996-02-15 1998-04-03 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes associees a un panneau amont
US5806302A (en) * 1996-09-24 1998-09-15 Rohr, Inc. Variable fan exhaust area nozzle for aircraft gas turbine engine with thrust reverser

Also Published As

Publication number Publication date
US9074554B2 (en) 2015-07-07
RU2538348C2 (ru) 2015-01-10
RU2012122102A (ru) 2013-12-10
EP2496817A1 (fr) 2012-09-12
CN102597475B (zh) 2014-12-03
FR2952128A1 (fr) 2011-05-06
FR2952128B1 (fr) 2011-11-04
WO2011055056A1 (fr) 2011-05-12
CN102597475A (zh) 2012-07-18
CA2776262A1 (fr) 2011-05-12
US20120193448A1 (en) 2012-08-02

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Legal Events

Date Code Title Description
B08F Application fees: dismissal - article 86 of industrial property law
B08K Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87)

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2433 DE 22-08-2017 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.