BRPI0907771A2 - Conjunto motor para aeronave, e, aeronave - Google Patents

Conjunto motor para aeronave, e, aeronave

Info

Publication number
BRPI0907771A2
BRPI0907771A2 BRPI0907771-5A BRPI0907771A BRPI0907771A2 BR PI0907771 A2 BRPI0907771 A2 BR PI0907771A2 BR PI0907771 A BRPI0907771 A BR PI0907771A BR PI0907771 A2 BRPI0907771 A2 BR PI0907771A2
Authority
BR
Brazil
Prior art keywords
aircraft
engine set
engine
Prior art date
Application number
BRPI0907771-5A
Other languages
English (en)
Inventor
Frédéric Journade
Delphine Jalbert
Original Assignee
Airbus Operations Sas
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 Airbus Operations Sas filed Critical Airbus Operations Sas
Publication of BRPI0907771A2 publication Critical patent/BRPI0907771A2/pt

Links

Classifications

    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BRPI0907771-5A 2008-02-28 2009-02-27 Conjunto motor para aeronave, e, aeronave BRPI0907771A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0851282A FR2928180B1 (fr) 2008-02-28 2008-02-28 Ensemble moteur pour aeronef comprenant une structure annulaire de transfert d'efforts entourant le carter central d'un turboreacteur.
PCT/FR2009/050324 WO2009112781A2 (fr) 2008-02-28 2009-02-27 Ensemble moteur pour aeronef comprenant une structure annulaire de transfert d'efforts entourant le carter central d'un turboreacteur

Publications (1)

Publication Number Publication Date
BRPI0907771A2 true BRPI0907771A2 (pt) 2015-07-14

Family

ID=39829016

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0907771-5A BRPI0907771A2 (pt) 2008-02-28 2009-02-27 Conjunto motor para aeronave, e, aeronave

Country Status (9)

Country Link
US (1) US8733693B2 (pt)
EP (1) EP2244943B1 (pt)
JP (1) JP5666317B2 (pt)
CN (1) CN101959758B (pt)
BR (1) BRPI0907771A2 (pt)
CA (1) CA2715734C (pt)
FR (1) FR2928180B1 (pt)
RU (1) RU2487058C2 (pt)
WO (1) WO2009112781A2 (pt)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2948635B1 (fr) * 2009-07-31 2011-08-26 Airbus Operations Sas Assemblage pour aeronef comprenant un mat d'accrochage de turbomachine dont les moyens d'attache sur la voilure sont agences en t
FR2950322B1 (fr) * 2009-09-22 2012-05-25 Airbus Operations Sas Element d'accrochage d'un moteur d'aeronef, ensemble d'aeronef comprenant cet element et aeronef associe
FR2950323B1 (fr) * 2009-09-22 2011-11-04 Airbus Operations Sas Mat d'accrochage de moteur d'aeronef, ensemble comprenant ce mat et aeronef associe
FR2963390B1 (fr) * 2010-07-30 2012-08-31 Snecma Turboreacteur lateral perfectionne pour limiter ses deformations
FR2994942B1 (fr) * 2012-09-06 2015-08-07 Airbus Operations Sas Ensemble propulsif lateral pour aeronef comprenant un arceau de support d'un turbomoteur.
FR2994941B1 (fr) * 2012-09-06 2015-08-07 Airbus Operations Sas Ensemble propulsif pour aeronef comprenant un carenage structural.
FR3000493A1 (fr) 2012-12-28 2014-07-04 Oribase Pharma Nouveaux inhibiteurs de proteines kinases
US20150121896A1 (en) * 2013-03-07 2015-05-07 United Technologies Corporation Reverse core flow engine mounting arrangement
FR3010147B1 (fr) * 2013-08-28 2015-08-21 Snecma Suspension isostatique d'un turboreacteur par double support arriere
FR3010047B1 (fr) * 2013-09-04 2017-03-31 Snecma Structure de liaison moteur-nacelle a platine a vis
FR3041935B1 (fr) * 2015-10-05 2017-12-15 Airbus Operations Sas Ensemble moteur pour aeronef comprenant au moins deux attaches moteur arriere decalees axialement l'une de l'autre
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
US10544793B2 (en) 2017-01-25 2020-01-28 General Electric Company Thermal isolation structure for rotating turbine frame
US10364705B2 (en) 2017-05-04 2019-07-30 United Technologies Corporation Strut assembly for bearing compartment
FR3106126B1 (fr) * 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine
US11613372B2 (en) * 2020-11-09 2023-03-28 Rohr, Inc. Ducted fan case attachment structure
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

Family Cites Families (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2965338A (en) * 1956-04-09 1960-12-20 Rolls Royce Engine mounting
US3540682A (en) * 1964-12-02 1970-11-17 Gen Electric Turbofan type engine frame and support system
GB1318748A (en) * 1970-08-11 1973-05-31 Secr Defence Gas turgine ducted fan engines for aircraft
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
FR2469566A1 (fr) 1979-11-12 1981-05-22 Snecma Perfectionnements aux dispositifs de fixation de turboreacteurs multiflux
FR2677953B1 (fr) 1991-06-19 1993-09-10 Snecma Structure de suspension arriere d'un turboreacteur.
FR2677954B1 (fr) * 1991-06-19 1993-09-10 Snecma Structure de suspension arriere du carter d'echappement d'un turboreacteur.
US5226288A (en) * 1991-06-21 1993-07-13 Rohr, Inc. Torque link fan jet engine support for reducing engine bending
RU2104228C1 (ru) * 1993-07-01 1998-02-10 Самарское государственное научно-производственное предприятие "Труд" Устройство для крепления авиационного двигателя к самолету
GB9602130D0 (en) * 1996-02-02 1996-04-03 Rolls Royce Plc Improved method of combining ducted fan gas turbine engine modules and aircraft structure
GB2394991B (en) * 2002-11-06 2006-02-15 Rolls Royce Plc Mounting arrangement
GB0328671D0 (en) * 2003-12-11 2004-01-14 Rolls Royce Plc Aircraft engine mounting
FR2868041B1 (fr) * 2004-03-25 2006-05-26 Snecma Moteurs Sa Suspension d'un moteur d'avion
FR2869874B1 (fr) * 2004-05-04 2006-06-23 Snecma Moteurs Sa Moteur d'avion avec des moyens de suspension a la structure d'un avion
FR2873986B1 (fr) * 2004-08-04 2007-12-21 Airbus France Sas Ensemble moteur pour aeronef
FR2873987B1 (fr) * 2004-08-05 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
GB0418454D0 (en) * 2004-08-19 2004-09-22 Rolls Royce Plc An engine mounting assembly
CN100575690C (zh) * 2005-09-12 2009-12-30 波音公司 包括锁定机构的反推力装置及其制造方法
FR2891244B1 (fr) 2005-09-26 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891243B1 (fr) 2005-09-26 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891245B1 (fr) 2005-09-26 2007-10-26 Airbus France Sas Procede de montage d'un moteur d'aeronef sur une structure rigide d'un mat d'accrochage du moteur
FR2891250B1 (fr) 2005-09-28 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
FR2891248B1 (fr) 2005-09-28 2009-05-01 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
FR2891251B1 (fr) 2005-09-28 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
GB0520850D0 (en) * 2005-10-14 2005-11-23 Rolls Royce Plc Fan static structure
GB0607991D0 (en) * 2006-04-22 2006-05-31 Rolls Royce Plc Aeroengine mounting
WO2008150202A1 (en) * 2007-06-08 2008-12-11 Volvo Aero Corporation A structure for transferring loads at a gas turbine engine, and an engine and an aircraft with such a structure
FR2928181B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant un turboreacteur avec des structures de renfort reliant le carter de soufflante au carter central.
FR2928136B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante.
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
US8567202B2 (en) * 2009-05-15 2013-10-29 Pratt & Whitney Canada Corp. Support links with lockable adjustment feature
US8313293B2 (en) * 2009-05-15 2012-11-20 Pratt & Whitney Canada Corp. Turbofan mounting system
FR2948636B1 (fr) * 2009-07-31 2012-01-13 Airbus Operations Sas Ensemble moteur pour aeronef dont le mat d'accrochage comprend une enveloppe structurale formant delimitation radiale interne du flux secondaire
US8621874B2 (en) * 2009-08-25 2014-01-07 Honeywell International Inc. Turbomachine core coupling assembly

Also Published As

Publication number Publication date
FR2928180A1 (fr) 2009-09-04
JP5666317B2 (ja) 2015-02-12
CA2715734C (fr) 2015-11-24
EP2244943B1 (fr) 2019-07-03
JP2011513630A (ja) 2011-04-28
RU2010139650A (ru) 2012-04-10
EP2244943A2 (fr) 2010-11-03
FR2928180B1 (fr) 2010-04-02
CN101959758B (zh) 2013-07-17
US8733693B2 (en) 2014-05-27
WO2009112781A3 (fr) 2009-11-05
WO2009112781A2 (fr) 2009-09-17
RU2487058C2 (ru) 2013-07-10
US20110290934A1 (en) 2011-12-01
CN101959758A (zh) 2011-01-26
CA2715734A1 (fr) 2009-09-17

Similar Documents

Publication Publication Date Title
BRPI0908079A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI0907771A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI0821929A2 (pt) Nacela para motor turbojato
BRPI0821504A2 (pt) nacela para motor de avião
BRPI0812844A2 (pt) Estribo de afixação para motor de aeronave, conjunto motor para aeronave, e, aeronave
BRPI0922745A2 (pt) ventoinha para turbomáquina de aeronave e turbomáquina para aeronave.
BRPI0717730A2 (pt) Nacela para motor turbojato de contorno, conjunto de propulsão e avião
BRPI0907959A2 (pt) Conjunto motor para aeronave, e, aeronave
BRPI0812818A2 (pt) Turbo-reator para aeronave
BRPI0907309A2 (pt) transmissão unidirecional para motor
DK2481143T3 (da) Motor
BRPI0820878A2 (pt) fuselagem com atenuação acústica para aeronave
DE602008005797D1 (de) Motor
DE602008000573D1 (de) Triebwerk
BRPI0821412A2 (pt) Configuração otimizada de motores para aeronave
BRPI1007029A2 (pt) conjunto de suspensão para motor turbojato de aeronaves
BRPI0810535A2 (pt) Nacela para turbojato e avião.
BRPI0822363A2 (pt) Nacela de motor turbojato
BRPI0822127A8 (pt) nacela para motor turbojato e aeronave
BR112014013202A2 (pt) estrutura acústica celular, especificamente para um motor turbojato, e motor turbojato
BRPI1009760A2 (pt) combustível para aviação.
ES2388023B2 (es) Dispositivo de escape para motor.
BRPI0914044A2 (pt) arranjo de entrada de ar para aeronave
DE602008002290D1 (de) Triebwerk
BRPI0921772A2 (pt) nacela de motor turbojato

Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 10A ANUIDADE.

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 2503 DE 26-12-2018 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.