DE602007003362D1 - Triebwerksanordnung für ein flugzeug mit stützgestell für eine auf zwei separaten elementen montierte lüfterhaube - Google Patents

Triebwerksanordnung für ein flugzeug mit stützgestell für eine auf zwei separaten elementen montierte lüfterhaube

Info

Publication number
DE602007003362D1
DE602007003362D1 DE602007003362T DE602007003362T DE602007003362D1 DE 602007003362 D1 DE602007003362 D1 DE 602007003362D1 DE 602007003362 T DE602007003362 T DE 602007003362T DE 602007003362 T DE602007003362 T DE 602007003362T DE 602007003362 D1 DE602007003362 D1 DE 602007003362D1
Authority
DE
Germany
Prior art keywords
plane
supporting frame
engine
fan cover
separate elements
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
DE602007003362T
Other languages
English (en)
Inventor
Frederic Roche
Jean-Marc Martinou
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
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 DE602007003362D1 publication Critical patent/DE602007003362D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • B64D27/402—
DE602007003362T 2006-07-11 2007-07-10 Triebwerksanordnung für ein flugzeug mit stützgestell für eine auf zwei separaten elementen montierte lüfterhaube Active DE602007003362D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0652910A FR2903665B1 (fr) 2006-07-11 2006-07-11 Ensemble moteur pour aeronef comprenant un berceau de support de capot de soufflante monte sur deux elements distincts
PCT/EP2007/057018 WO2008006823A1 (fr) 2006-07-11 2007-07-10 Ensemble moteur pour aeronef comprenant un berceau de support de capot de soufflante monte sur deux elements distincts

Publications (1)

Publication Number Publication Date
DE602007003362D1 true DE602007003362D1 (de) 2009-12-31

Family

ID=37685728

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007003362T Active DE602007003362D1 (de) 2006-07-11 2007-07-10 Triebwerksanordnung für ein flugzeug mit stützgestell für eine auf zwei separaten elementen montierte lüfterhaube

Country Status (11)

Country Link
US (1) US8356769B2 (de)
EP (1) EP2038175B1 (de)
JP (1) JP5479892B2 (de)
CN (1) CN101489871B (de)
AT (1) ATE449001T1 (de)
BR (1) BRPI0714029A2 (de)
CA (1) CA2657397C (de)
DE (1) DE602007003362D1 (de)
FR (1) FR2903665B1 (de)
RU (1) RU2429168C2 (de)
WO (1) WO2008006823A1 (de)

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BRPI0717730A2 (pt) * 2006-10-11 2013-10-22 Aircelle Sa Nacela para motor turbojato de contorno, conjunto de propulsão e avião
FR2920409B1 (fr) * 2007-08-27 2009-12-18 Airbus France Berceau de support de capot de soufflante monte sur le mat d'accrochage et sur l'entree d'air de la nacelle
FR2926788B1 (fr) * 2008-01-25 2010-04-02 Snecma Fixation d'un turboreacteur multiflux a un aeronef
JP5642379B2 (ja) * 2009-12-01 2014-12-17 三菱航空機株式会社 航空機のエンジンマウント、航空機
FR2960216B1 (fr) * 2010-05-19 2013-02-15 Aircelle Sa Element d'aerodynamisme pour une nacelle d'aeronef
US8727269B2 (en) * 2011-06-06 2014-05-20 General Electric Company System and method for mounting an aircraft engine
GB2492107B (en) * 2011-06-22 2013-09-04 Rolls Royce Plc Mounting assembly
FR2978730B1 (fr) * 2011-08-03 2013-09-27 Airbus Operations Sas Berceau d'articulation de capots de soufflante supportes par ces capots en position fermee
FR2979613B1 (fr) * 2011-09-01 2014-06-13 Snecma Ensemble forme par un turbomoteur et son systeme d'attache a une structure d'aeronef
CN102392915A (zh) * 2011-11-04 2012-03-28 哈尔滨飞机工业集团有限责任公司 一种用于飞机机翼外挂电缆的挂架
CN102849218A (zh) * 2012-09-04 2013-01-02 西安飞机工业（集团）有限责任公司 一种飞机辅助动力装置安装梁
US8979020B2 (en) * 2013-06-07 2015-03-17 Pratt & Whitney Canada Corp. Mounting system for mounting engine nacelle components and associated method
US10144524B2 (en) * 2013-06-14 2018-12-04 Rohr, Inc. Assembly for mounting a turbine engine to a pylon
CN105392700B (zh) 2013-07-26 2018-12-18 Mra系统有限责任公司 飞行器发动机吊架
US10252790B2 (en) * 2016-08-11 2019-04-09 General Electric Company Inlet assembly for an aircraft aft fan
US10259565B2 (en) * 2016-08-11 2019-04-16 General Electric Company Inlet assembly for an aircraft aft fan
US11267578B2 (en) * 2017-06-19 2022-03-08 Rohr, Inc. Hinge assembly
FR3089954B1 (fr) * 2018-12-12 2021-01-08 Airbus Operations Sas Ensemble de motorisation pour un aeronef comprenant un support de charge
FR3096352B1 (fr) 2019-05-24 2021-06-11 Airbus Operations Sas Ensemble de motorisation pour un aeronef comprenant un support de charge
US11548653B2 (en) * 2019-10-08 2023-01-10 Rohr, Inc. Support structure for inner cowls of an aircraft propulsion system
CN112124606B (zh) * 2020-09-30 2022-07-05 中航(成都)无人机系统股份有限公司 一种可模块化组装的机载吊舱

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US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
US4458863A (en) * 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
US4471609A (en) * 1982-08-23 1984-09-18 The Boeing Company Apparatus and method for minimizing engine backbone bending
US4697763A (en) * 1985-10-31 1987-10-06 The Boeing Company Hinge system for thrust reverser cowl
US5054715A (en) * 1988-11-10 1991-10-08 The Boeing Company Apparatus and methods for reducing aircraft lifting surface flutter
US4917331A (en) * 1988-11-10 1990-04-17 The Boeing Company Apparatus and methods for reducing aircraft lifting surface flutter
FR2661213B1 (fr) * 1990-04-19 1992-07-03 Snecma Moteur d'aviation a tres grand taux de dilution et du type dit contrafan avant.
GB2266080A (en) * 1992-04-16 1993-10-20 Rolls Royce Plc Mounting arrangement for a gas turbine engine.
FR2732074B1 (fr) * 1995-03-21 1997-06-06 Aerospatiale Turboreacteur a double flux a nacelle flottante
US6039287A (en) * 1996-08-02 2000-03-21 Alliedsignal Inc. Detachable integral aircraft tailcone and power assembly
FR2771710B1 (fr) * 1997-12-03 2000-02-11 Aerospatiale Dispositif d'ouverture commun a deux capots adjacents de nacelle de moteur d'avion
FR2772342B1 (fr) * 1997-12-16 2000-02-18 Aerospatiale Ensemble propulseur a capots de soufflante munis de securites de maintien et de positionnement, pour aeronef
US6126110A (en) * 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon
FR2775465B1 (fr) * 1998-03-02 2000-05-26 Aerospatiale Dispositif d'accrochage d'un moteur sur un pylone d'aeronef
US6131850A (en) * 1998-06-12 2000-10-17 The Boeing Company Adjustable length brace for cyclic loads
FR2851226B1 (fr) * 2003-02-19 2005-05-20 Snecma Moteurs Structure porteuse pour un turbopropulseur et ensemble comportant une telle structure porteuse
GB0320371D0 (en) * 2003-08-29 2003-10-01 Rolls Royce Plc A closure panel arrangement
US7104306B2 (en) * 2004-06-14 2006-09-12 The Boeing Company Cast unitized primary truss structure and method
GB0608983D0 (en) * 2006-05-06 2006-06-14 Rolls Royce Plc Aeroengine mount

Also Published As

Publication number Publication date
RU2009104478A (ru) 2010-08-20
ATE449001T1 (de) 2009-12-15
US20090266932A1 (en) 2009-10-29
CA2657397A1 (en) 2008-01-17
WO2008006823A1 (fr) 2008-01-17
JP5479892B2 (ja) 2014-04-23
EP2038175B1 (de) 2009-11-18
EP2038175A1 (de) 2009-03-25
US8356769B2 (en) 2013-01-22
CN101489871A (zh) 2009-07-22
JP2009542517A (ja) 2009-12-03
FR2903665A1 (fr) 2008-01-18
RU2429168C2 (ru) 2011-09-20
CN101489871B (zh) 2011-05-11
CA2657397C (en) 2014-03-25
FR2903665B1 (fr) 2008-10-10
BRPI0714029A2 (pt) 2012-12-18

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Legal Events

Date Code Title Description
8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS OPERATIONS, TOULOUSE, FR

8364 No opposition during term of opposition