BR112013010654A2 - nacela de motor turbojato compreendendo uma estrutura fixa - Google Patents

nacela de motor turbojato compreendendo uma estrutura fixa

Info

Publication number
BR112013010654A2
BR112013010654A2 BR112013010654A BR112013010654A BR112013010654A2 BR 112013010654 A2 BR112013010654 A2 BR 112013010654A2 BR 112013010654 A BR112013010654 A BR 112013010654A BR 112013010654 A BR112013010654 A BR 112013010654A BR 112013010654 A2 BR112013010654 A2 BR 112013010654A2
Authority
BR
Brazil
Prior art keywords
fixed structure
engine compartment
turbojet engine
turbojet
compartment
Prior art date
Application number
BR112013010654A
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 BR112013010654A2 publication Critical patent/BR112013010654A2/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • 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
    • 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
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BR112013010654A 2010-11-16 2011-11-03 nacela de motor turbojato compreendendo uma estrutura fixa BR112013010654A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1059392A FR2967398B1 (fr) 2010-11-16 2010-11-16 Structure de renforcement d'une nacelle de turboreacteur
PCT/FR2011/052564 WO2012066211A1 (fr) 2010-11-16 2011-11-03 Structure de renforcement d'une nacelle de turboréacteur

Publications (1)

Publication Number Publication Date
BR112013010654A2 true BR112013010654A2 (pt) 2016-08-09

Family

ID=44149010

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013010654A BR112013010654A2 (pt) 2010-11-16 2011-11-03 nacela de motor turbojato compreendendo uma estrutura fixa

Country Status (8)

Country Link
US (1) US10087842B2 (pt)
EP (1) EP2640639B1 (pt)
CN (1) CN103209893B (pt)
BR (1) BR112013010654A2 (pt)
CA (1) CA2816455A1 (pt)
FR (1) FR2967398B1 (pt)
RU (1) RU2569725C2 (pt)
WO (1) WO2012066211A1 (pt)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9404507B2 (en) * 2013-04-15 2016-08-02 Mra Systems, Inc. Inner cowl structure for aircraft turbine engine
FR3009339B1 (fr) * 2013-07-30 2018-01-26 Safran Aircraft Engines Turbomachine comprenant un dispositif de refroidissement du pylone
US9771894B2 (en) * 2013-10-07 2017-09-26 Rohr, Inc. Radially connected cascade grids
FR3047973B1 (fr) * 2016-02-23 2018-03-09 Airbus Operations Ensemble moteur pour aeronef, comprenant un dispositif d'accrochage du moteur equipe de capots mobiles structuraux relies au caisson central
FR3065710A1 (fr) * 2017-04-27 2018-11-02 Airbus Operations Procede d'etalonnage par mesure de la rigidite de structures de support d'un modele comportant une structure principale et au moins une structure de support
FR3075886B1 (fr) * 2017-12-22 2019-12-27 Safran Nacelles Nacelle de turboreacteur comportant des ouvertures de capots avant d'acces a des points de fixation de la nacelle
FR3088373B1 (fr) * 2018-11-09 2021-03-19 Safran Nacelles Joint d’etancheite pour nacelle de turboreacteur d’aeronef
FR3096741B1 (fr) * 2019-05-28 2022-11-18 Safran Nacelles Ensemble propulsif d’aéronef
US11268406B2 (en) * 2019-08-12 2022-03-08 The Boeing Company Movement-limiting device for a turbine engine and associated method
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

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3500646A (en) * 1968-04-19 1970-03-17 Rohr Corp Thrust reverser
GB1583952A (en) * 1976-07-13 1981-02-04 Short Brothers & Harland Ltd Gas turbine engines
US5046689A (en) * 1989-04-19 1991-09-10 The Boeing Company Cowling interlock system
FR2762875B1 (fr) * 1997-04-30 1999-06-04 Hispano Suiza Sa Inverseur de poussee protege en cas de deverrouillage accidentel
FR2856379B1 (fr) * 2003-06-18 2006-11-24 Airbus France Moteur d'avion dont les capots de soufflante et d'inverseurs de poussee sont separes par un jeu reduit
FR2896481B1 (fr) * 2006-01-23 2009-12-04 Aircelle Sa Systeme de fixation pour element constitutif d'une nacelle de turboreacteur
EP2076438A2 (fr) * 2006-10-11 2009-07-08 Aircelle Nacelle pour turboréacteur double flux
FR2908152B1 (fr) * 2006-11-08 2009-02-06 Snecma Sa Aube en fleche de turbomachine
FR2915527B1 (fr) * 2007-04-30 2009-06-12 Aircelle Sa Structure arriere de nacelle pour moteur a reacteur, telle qu'un inverseur de poussee
FR2925607B1 (fr) * 2007-12-21 2013-05-10 Aircelle Sa Nacelle pour moteur d'aeronef a tuyere de section variable
RU2509649C1 (ru) * 2012-11-01 2014-03-20 Открытое акционерное общество Центральный научно-исследовательский институт специального машиностроения Способ изготовления секций несущей решетки реверсера тяги самолета из полимерных композиционных материалов, оправка для осуществления способа изготовления секций несущей решетки реверсера тяги самолета из полимерных композиционных материалов, форма для заливки антиадгезионного эластичного материала разделительного слоя оправки для осуществления способа изготовления секций несущей решетки реверсера тяги самолета из полимерных композиционных материалов и секция несущей решетки реверсера тяги самолета из полимерных композиционных материалов

Also Published As

Publication number Publication date
RU2013126748A (ru) 2014-12-27
US20130243589A1 (en) 2013-09-19
US10087842B2 (en) 2018-10-02
CA2816455A1 (fr) 2012-05-24
FR2967398B1 (fr) 2012-11-02
CN103209893A (zh) 2013-07-17
FR2967398A1 (fr) 2012-05-18
RU2569725C2 (ru) 2015-11-27
WO2012066211A1 (fr) 2012-05-24
EP2640639B1 (fr) 2015-12-30
EP2640639A1 (fr) 2013-09-25
CN103209893B (zh) 2015-08-12

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
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 2435 DE 05-09-2017 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.