BR112012011079A2 - montagem para um motor turbojato de aviao compreendendo uma carenagem de reversao de empuxo - Google Patents

montagem para um motor turbojato de aviao compreendendo uma carenagem de reversao de empuxo

Info

Publication number
BR112012011079A2
BR112012011079A2 BR112012011079A BR112012011079A BR112012011079A2 BR 112012011079 A2 BR112012011079 A2 BR 112012011079A2 BR 112012011079 A BR112012011079 A BR 112012011079A BR 112012011079 A BR112012011079 A BR 112012011079A BR 112012011079 A2 BR112012011079 A2 BR 112012011079A2
Authority
BR
Brazil
Prior art keywords
fairing
assembly
turbojet engine
pylon
thrust reversing
Prior art date
Application number
BR112012011079A
Other languages
English (en)
Inventor
André Baillard
Guy Bernard Vauchel
Jean-Philippe Joret
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 BR112012011079A2 publication Critical patent/BR112012011079A2/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
    • F02K1/76—Control or regulation of thrust reversers
    • F02K1/766—Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/06—Attaching of nacelles, fairings or cowlings

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Wind Motors (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

montagem para um motor turbojato de avião compreendendo uma carenagem de reversão de empuxo. a invenção refere-se a uma montagem para um motor turbojato que inclui um pilone (1) e uma nacela suportada por referido pilone (1). referida nacela (3) inclui um reversor de empuxo com grade (21) incluindo uma carenagem integral montada de modo a deslizar sobre os trilhos (15), que são dispostos em ambos os lados do referido pilone (1), entre uma posição de jato direto e uma posição de reversão de empuxo. referida montagem é caracterizada pelo fato de que inclui meios (23,31) para bloquear o movimento deslizante da carenagem sobre os trilhos (15), referidos meios sendo inseridos entre o pilone (1) e a carenagem.
BR112012011079A 2009-11-26 2010-11-25 montagem para um motor turbojato de aviao compreendendo uma carenagem de reversao de empuxo BR112012011079A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0905687A FR2952908B1 (fr) 2009-11-26 2009-11-26 Ensemble pour turboreacteur d'aeronef
PCT/FR2010/052537 WO2011067520A1 (fr) 2009-11-26 2010-11-25 Ensemble pour turboreacteur d'aeronef comprenant un capot d'inversion de pousee

Publications (1)

Publication Number Publication Date
BR112012011079A2 true BR112012011079A2 (pt) 2016-07-05

Family

ID=42289473

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012011079A BR112012011079A2 (pt) 2009-11-26 2010-11-25 montagem para um motor turbojato de aviao compreendendo uma carenagem de reversao de empuxo

Country Status (9)

Country Link
US (1) US9249756B2 (pt)
EP (1) EP2504554B1 (pt)
CN (1) CN102630272A (pt)
BR (1) BR112012011079A2 (pt)
CA (1) CA2780058A1 (pt)
ES (1) ES2555391T3 (pt)
FR (1) FR2952908B1 (pt)
RU (1) RU2582370C2 (pt)
WO (1) WO2011067520A1 (pt)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2978494B1 (fr) 2011-07-25 2013-08-02 Aircelle Sa Dispositif de liaison d'un cadre avant a un carter de soufflante
FR2978991A1 (fr) * 2011-08-08 2013-02-15 Snecma Dispositif d'inversion de poussee pour tuyere compacte
FR2981989B1 (fr) 2011-10-31 2013-11-01 Aircelle Sa Inverseur de poussee a grilles mobiles et capot mobile monobloc
FR2991668B1 (fr) * 2012-06-08 2014-06-20 Aircelle Sa Dispositif de verrouillage/deverrouillage pour capot monobloc d'inverseur de poussee de nacelle de turboreacteur
FR2991670B1 (fr) * 2012-06-12 2014-06-20 Aircelle Sa Inverseur de poussee a grilles retractables et tuyere variable
CN103101628B (zh) 2013-02-06 2015-05-27 中国商用飞机有限责任公司 一种与飞机吊挂一体化的前安装节
CN103112595B (zh) * 2013-02-06 2016-01-27 中国商用飞机有限责任公司 推进系统一体化的吊挂结构
FR3003305B1 (fr) * 2013-03-15 2015-03-27 Aircelle Sa Dispositif d'inhibition mecanique integre a une ligne de defense d'un inverseur de poussee
FR3011039B1 (fr) * 2013-09-23 2018-02-16 Safran Nacelles Inverseur de poussee pour une nacelle de turboreacteur, comprenant une butee de fin de course sur le rail de guidage primaire
US9689345B2 (en) 2015-06-10 2017-06-27 Woodward, Inc. Electric track lock
FR3038587B1 (fr) * 2015-07-10 2019-05-17 Safran Nacelles Nacelle de turboreacteur d’aeronef, ensemble propulsif comportant une nacelle, et aeronef comportant au moins un ensemble propulsif
US10428763B2 (en) * 2016-04-01 2019-10-01 Rohr, Inc. Controlling a relative position at an interface between translating structures of an aircraft nacelle
US10294893B2 (en) 2016-05-25 2019-05-21 Honeywell International Inc. System and method for monitoring a translating cowl thrust reverser
US10543927B2 (en) 2016-11-18 2020-01-28 Rohr, Inc. Lockable track system for a translating nacelle structure
US10738737B2 (en) 2016-11-18 2020-08-11 Rohr, Inc. Self-locking alignment at a nacelle interface
UA117948U (uk) * 2017-02-23 2017-07-10 Державне Підприємство "Запорізьке Машинобудівне Конструкторське Бюро "Прогрес" Імені Академіка О.Г. Івченка" Реверсивний пристрій турбореактивного двигуна
US11085395B2 (en) * 2017-12-22 2021-08-10 Airbus Operations S.A.S. Nacelle system and methods of operation
FR3085726B1 (fr) * 2018-09-07 2020-12-11 Safran Nacelles Inverseur de poussee a structure mobile en c pour ensemble propulsif d’aeronef, et procede de maintenance s’y rapportant
US11441514B2 (en) 2018-10-02 2022-09-13 Woodward, Inc. Tertiary lock
US10865738B2 (en) 2019-02-27 2020-12-15 Woodward, Inc. Traveling finger lock for an actuator
FR3128207A1 (fr) * 2021-10-15 2023-04-21 Airbus Operations Turboréacteur double flux comportant des déflecteurs mobiles et un système d’actionnement des déflecteurs
CN113928573B (zh) * 2021-11-19 2023-04-18 中国直升机设计研究所 一种具备导向缓冲功能的滑动整流罩
US11788490B1 (en) 2022-12-05 2023-10-17 Woodward, Inc. Traveling finger lock for an actuator

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2494775B1 (fr) * 1980-11-27 1985-07-05 Astech Dispositif pour la commande d'un inverseur de poussee pour moteur a reaction
GB9418895D0 (en) * 1994-09-20 1994-11-09 Lucas Ind Plc Lock mechanism
FR2756868B1 (fr) * 1996-12-05 1999-01-08 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes maintenues dans les lignes de nacelle
FR2765916B1 (fr) * 1997-07-10 1999-08-20 Hispano Suiza Sa Inverseur de poussee a resistance amelioree aux impacts
US6021636A (en) * 1997-07-25 2000-02-08 Alliedsignal Inc. Lightweight tertiary thrust reverser lock assembly with a blocking member
US6584763B2 (en) * 2001-08-01 2003-07-01 Rohr, Inc. Lock for the translating sleeve of a turbofan engine thrust reverser
FR2830051B1 (fr) * 2001-09-27 2003-11-07 Hurel Hispano Le Havre Systeme de verrouillage sur un inverseur de poussee a grilles
US7409820B2 (en) * 2004-11-16 2008-08-12 Honeywell International Inc. Electrical thrust reverser tertiary lock system including a voltage limiting circuit
US7484356B1 (en) * 2005-07-26 2009-02-03 Aeronautical Concepts Of Exhaust, Llc Cascade reverser without blocker doors
EP1764499B1 (en) * 2005-09-14 2017-12-13 The Boeing Company Thrust reverser including a latching mechanism and method of operating a latching mechanism of a thrust reverser
FR2914700B1 (fr) * 2007-04-04 2009-05-22 Aircelle Sa Inverseur de poussee pour moteur a reaction
FR2916426B1 (fr) * 2007-05-22 2010-04-02 Aircelle Sa Ensemble arriere de nacelle pour turboreacteur.

Also Published As

Publication number Publication date
CN102630272A (zh) 2012-08-08
US20120228403A1 (en) 2012-09-13
RU2012125378A (ru) 2014-01-10
RU2582370C2 (ru) 2016-04-27
FR2952908B1 (fr) 2011-11-25
US9249756B2 (en) 2016-02-02
ES2555391T3 (es) 2015-12-30
CA2780058A1 (fr) 2011-06-09
EP2504554A1 (fr) 2012-10-03
WO2011067520A1 (fr) 2011-06-09
EP2504554B1 (fr) 2015-09-09
FR2952908A1 (fr) 2011-05-27

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Legal Events

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B08F Application fees: application dismissed [chapter 8.6 patent gazette]

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B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2386 DE 27-09-2016 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.

B350 Update of information on the portal [chapter 15.35 patent gazette]