BRPI0815704A2 - Dispositivo de afixação de um motor de aeronave, conjunto motor, e, aeronave. - Google Patents

Dispositivo de afixação de um motor de aeronave, conjunto motor, e, aeronave.

Info

Publication number
BRPI0815704A2
BRPI0815704A2 BRPI0815704-9A2A BRPI0815704A BRPI0815704A2 BR PI0815704 A2 BRPI0815704 A2 BR PI0815704A2 BR PI0815704 A BRPI0815704 A BR PI0815704A BR PI0815704 A2 BRPI0815704 A2 BR PI0815704A2
Authority
BR
Brazil
Prior art keywords
aircraft
engine
positioning device
assembly
engine assembly
Prior art date
Application number
BRPI0815704-9A2A
Other languages
English (en)
Inventor
Emmanuel Guillet
Jean-Marc Martinou
Pascal Gardes
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 BRPI0815704A2 publication Critical patent/BRPI0815704A2/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
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
  • Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
  • Catching Or Destruction (AREA)
  • Body Structure For Vehicles (AREA)
BRPI0815704-9A2A 2007-08-24 2008-08-22 Dispositivo de afixação de um motor de aeronave, conjunto motor, e, aeronave. BRPI0815704A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0757166A FR2920138B1 (fr) 2007-08-24 2007-08-24 Dispositif d'accrochage de moteur d'aeronef comportant un dispositif de reprise des efforts de poussee a encombrement reduit
PCT/EP2008/061010 WO2009027333A1 (fr) 2007-08-24 2008-08-22 Dispositif d'accrochage de moteur d'aeronef comportant un dispositif de reprise des efforts de poussee a encombrement reduit

Publications (1)

Publication Number Publication Date
BRPI0815704A2 true BRPI0815704A2 (pt) 2015-02-10

Family

ID=39356550

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0815704-9A2A BRPI0815704A2 (pt) 2007-08-24 2008-08-22 Dispositivo de afixação de um motor de aeronave, conjunto motor, e, aeronave.

Country Status (9)

Country Link
US (1) US8256708B2 (pt)
EP (1) EP2181037B1 (pt)
JP (1) JP5421263B2 (pt)
CN (1) CN101784442B (pt)
BR (1) BRPI0815704A2 (pt)
CA (1) CA2696802C (pt)
FR (1) FR2920138B1 (pt)
RU (1) RU2472676C2 (pt)
WO (1) WO2009027333A1 (pt)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2915175B1 (fr) * 2007-04-20 2009-07-17 Airbus France Sa Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere deportee du caisson
FR2918644B1 (fr) * 2007-07-09 2009-10-23 Airbus France Sas Mat d'accrochage de moteur pour aeronef disposant d'un palonnier articule en quatre points.
US8128021B2 (en) * 2008-06-02 2012-03-06 United Technologies Corporation Engine mount system for a turbofan gas turbine engine
US8807477B2 (en) 2008-06-02 2014-08-19 United Technologies Corporation Gas turbine engine compressor arrangement
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8695920B2 (en) 2008-06-02 2014-04-15 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8800914B2 (en) 2008-06-02 2014-08-12 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8511605B2 (en) 2008-06-02 2013-08-20 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
GB0810585D0 (en) * 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
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
DE102009054568A1 (de) 2009-12-11 2011-06-16 Rolls-Royce Deutschland Ltd & Co Kg Vorrichtung zur Aufhängung eines Strahltriebwerks an einer Stützstruktur
FR2959210B1 (fr) 2010-04-21 2013-08-23 Snecma Palonnier de suspension de turboreacteur d'aeronef et suspension avec accroche-soufflante ainsi equipee
FR2961172B1 (fr) * 2010-06-14 2012-07-27 Snecma Suspension d'un turbomoteur ou analogue a un pylone d'aeronef, a securite integree.
FR2962976B1 (fr) * 2010-07-22 2013-07-26 Airbus Operations Sas Dispositif de liaison destine a relier un premier corps a un second corps, notamment pour ensemble moteur d'aeronef
FR2965549B1 (fr) * 2010-10-01 2013-07-05 Airbus Operations Sas Dispositif de reprise de poussee a bielles pour mat d'accrochage d'un moteur d'aeronef, integrant trois rotules alignees
FR2969578B1 (fr) * 2010-12-27 2013-02-08 Snecma Dispositif de suspension d'un turboreacteur
FR2973345B1 (fr) * 2011-03-29 2013-04-05 Airbus Dispositif de pose et de depose d'un pre-refroidisseur d'un moteur d'aeronef
CN103032434B (zh) * 2012-11-26 2016-05-04 中国商用飞机有限责任公司 破损安全保险销
FR3000529B1 (fr) * 2012-12-28 2015-03-06 Airbus Operations Sas Dispositif de liaison souple pour ensemble propulsif d'aeronef
FR3002288B1 (fr) * 2013-02-20 2022-11-25 Snecma Suspension d'un turboreacteur par double support arriere
EP3058202A4 (en) 2013-10-16 2017-06-28 United Technologies Corporation Geared turbofan engine with targeted modular efficiency
FR3015434B1 (fr) * 2013-12-23 2017-12-08 Snecma Suspension de turbomachine
CN107108039B (zh) * 2015-01-07 2019-08-30 洛德公司 飞行器发动机安装架
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
FR3069848B1 (fr) * 2017-08-02 2019-08-30 Airbus Structure primaire allegee pour mat d'accrochage de moteur d'aeronef
EP3663206B1 (en) * 2018-12-06 2023-09-06 AIRBUS HELICOPTERS DEUTSCHLAND GmbH An attachment for suspending an aircraft engine
US11479104B2 (en) 2019-07-24 2022-10-25 Honeywell International Inc. System and method for gas turbine engine mount with seal
FR3128205A1 (fr) 2021-10-14 2023-04-21 Airbus Operations Assemblage d’un mat avec un moteur d’un aéronef
CN113859553A (zh) * 2021-11-18 2021-12-31 中国商用飞机有限责任公司 飞行器吊挂接口组件及飞行器吊挂

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
US5725181A (en) * 1996-05-01 1998-03-10 The Boeing Company Aircraft engine thrust mount
US5873547A (en) * 1997-05-20 1999-02-23 The Boeing Company Aircraft engine thrust mount
US6189830B1 (en) * 1999-02-26 2001-02-20 The Boeing Company Tuned engine mounting system for jet aircraft
FR2799432A1 (fr) * 1999-10-07 2001-04-13 Snecma Suspension a securite integree pour groupes motopropulseurs d'aeronefs
FR2806699B1 (fr) * 2000-03-22 2002-05-10 Aerospatiale Matra Airbus Dispositif de reprise de poussee apte a relier un turbomoteur et un mat d'aeronef
FR2828167B1 (fr) * 2001-07-31 2003-11-21 Airbus France Dispositif d'accrochage d'un moteur sur un aeronef
DE10249517B4 (de) * 2002-10-23 2008-11-20 Eurocopter Deutschland Gmbh Stoßabsorbierende, lastbegrenzende Verbindungsvorrichtung sowie Drehflügelflugzeug mit einer solchen Verbindungsvorrichtung
JP3953409B2 (ja) * 2002-10-31 2007-08-08 スネクマ ジェットエンジンの懸架装置
FR2855496B1 (fr) * 2003-05-27 2006-09-22 Snecma Moteurs Suspension arriere de moteur d'avion avec reprise de poussee
FR2856656B1 (fr) * 2003-06-30 2006-12-01 Snecma Moteurs Suspension arriere de moteur d'avion avec bielles de reprise de poussee et palonnier en forme de boomerang
RU2252176C1 (ru) * 2003-11-27 2005-05-20 Открытое акционерное общество "Туполев" (ОАО "Туполев") Устройство крепления авиационного двигателя летательного аппарата
FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
FR2887851B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2887850B1 (fr) * 2005-06-29 2008-11-07 Airbus France Sas Dispositif d'accrochage d'un moteur interpose entre une voilure d'aeronef et ledit moteur
FR2891244B1 (fr) * 2005-09-26 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891251B1 (fr) * 2005-09-28 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2903382B1 (fr) * 2006-07-10 2008-10-10 Airbus France Sas Dispositif d'accrochage d'un moteur d'aeronef comportant deux bielles de reprise de poussee a emboitement transversal
FR2914908B1 (fr) 2007-04-13 2009-10-30 Airbus France Sa Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif.

Also Published As

Publication number Publication date
WO2009027333A1 (fr) 2009-03-05
EP2181037A1 (fr) 2010-05-05
RU2472676C2 (ru) 2013-01-20
US20110114786A1 (en) 2011-05-19
US8256708B2 (en) 2012-09-04
CA2696802A1 (fr) 2009-03-05
JP5421263B2 (ja) 2014-02-19
JP2010536643A (ja) 2010-12-02
CN101784442A (zh) 2010-07-21
CN101784442B (zh) 2013-10-09
FR2920138B1 (fr) 2010-03-12
RU2010111152A (ru) 2011-09-27
EP2181037B1 (fr) 2012-06-20
FR2920138A1 (fr) 2009-02-27
CA2696802C (fr) 2015-11-24

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06T Formal requirements before examination [chapter 6.20 patent gazette]
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 11A 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 2529 DE 25-06-2019 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.