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DE602007002714D1 - Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel - Google Patents

Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel

Info

Publication number
DE602007002714D1
DE602007002714D1 DE602007002714T DE602007002714T DE602007002714D1 DE 602007002714 D1 DE602007002714 D1 DE 602007002714D1 DE 602007002714 T DE602007002714 T DE 602007002714T DE 602007002714 T DE602007002714 T DE 602007002714T DE 602007002714 D1 DE602007002714 D1 DE 602007002714D1
Authority
DE
Germany
Prior art keywords
turbine engine
fan casing
mast
cladding
mounting
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
DE602007002714T
Other languages
English (en)
Inventor
Alain Porte
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 DE602007002714D1 publication Critical patent/DE602007002714D1/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; 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Toys (AREA)
  • Catching Or Destruction (AREA)
  • Micromachines (AREA)
  • Tires In General (AREA)
DE602007002714T 2006-06-20 2007-06-18 Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel Active DE602007002714D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0605448A FR2902406B1 (fr) 2006-06-20 2006-06-20 Carenage pour mat de suspension d'un turbomoteur a une aile d'aeronef
PCT/FR2007/001009 WO2007147965A2 (fr) 2006-06-20 2007-06-18 Carenage pour mat de suspension d'un turbomoteur a une aile d'aeronef

Publications (1)

Publication Number Publication Date
DE602007002714D1 true DE602007002714D1 (de) 2009-11-19

Family

ID=37726661

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007002714T Active DE602007002714D1 (de) 2006-06-20 2007-06-18 Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel

Country Status (11)

Country Link
US (1) US8366039B2 (de)
EP (1) EP2029429B1 (de)
JP (1) JP5097772B2 (de)
CN (1) CN101472797B (de)
AT (1) ATE444896T1 (de)
BR (1) BRPI0712635A2 (de)
CA (1) CA2653067C (de)
DE (1) DE602007002714D1 (de)
FR (1) FR2902406B1 (de)
RU (1) RU2391260C1 (de)
WO (1) WO2007147965A2 (de)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8769924B2 (en) * 2008-05-30 2014-07-08 United Technologies Corporation Gas turbine engine assembly including accessory components within the nacelle
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
FR2961173B1 (fr) 2010-06-09 2012-06-22 Airbus Operations Sas Nacelle incorporant une entree d'air au niveau d'une casquette
CN102826218B (zh) * 2012-09-11 2016-06-15 江西洪都航空工业集团有限责任公司 一种双发飞机后体整流结构
US9404507B2 (en) * 2013-04-15 2016-08-02 Mra Systems, Inc. Inner cowl structure for aircraft turbine engine
CA2918320C (en) 2013-07-26 2018-05-15 Mra Systems, Inc. Aircraft engine pylon
CN103569367B (zh) * 2013-11-13 2015-08-26 中国航空工业集团公司西安飞机设计研究所 机翼吊装涡扇发动机飞机的发动机挂架
US9656761B2 (en) 2014-04-30 2017-05-23 The Boeing Company Lipskin for a nacelle and methods of making the same
US9938852B2 (en) 2014-04-30 2018-04-10 The Boeing Company Noise attenuating lipskin assembly and methods of assembling the same
US9708072B2 (en) 2014-04-30 2017-07-18 The Boeing Company Aircraft engine nacelle bulkheads and methods of assembling the same
US9604438B2 (en) 2014-04-30 2017-03-28 The Boeing Company Methods and apparatus for noise attenuation in an engine nacelle
US20150321766A1 (en) * 2014-05-06 2015-11-12 The Boeing Company Nacelle-To-Pylon Fairing
JP6437347B2 (ja) * 2015-02-27 2018-12-12 三菱重工業株式会社 推力発生装置及び航空機
US20160356180A1 (en) * 2015-06-03 2016-12-08 The Boeing Company Nacelle inlet having an angle or curved aft bulkhead
FR3040043B1 (fr) * 2015-08-12 2019-04-12 Sogeclair Sa Mat de moteur d'aeronef a ossature multifonctionnelle integree
US9896217B2 (en) * 2016-01-07 2018-02-20 The Boeing Company Enhanced performance jet engine mounting struts
US10611490B2 (en) * 2016-11-02 2020-04-07 Rohr, Inc. Fan cowl fairing restraining system
FR3079215B1 (fr) * 2018-03-22 2020-11-20 Airbus Operations Sas Carenage avant d'un mat d'aeronef comprenant une coiffe mobile et aeronef equipe dudit carenage avant
FR3085353A1 (fr) * 2018-09-04 2020-03-06 Airbus Operations Ensemble turbomachine d'aeronef comportant un capot articule
CN109163624B (zh) * 2018-09-27 2024-02-13 宁波天擎航天科技有限公司 一种可分离的火箭推进系统
FR3090581A1 (fr) 2018-12-21 2020-06-26 Airbus Operations (S.A.S.) Ensemble propulsif d’un aéronef comprenant un carénage de jonction entre une nacelle et un mât de l’aéronef équipé d’un capot amovible et aéronef équipé dudit ensemble propulsif
CN110439707B (zh) * 2019-07-26 2021-10-01 中国航发沈阳发动机研究所 一种飞机尾部弹性片组件
FR3122694B1 (fr) * 2021-05-07 2024-03-29 Safran Aircraft Engines Turboréacteur muni d’un ensemble de fixation disposé sur un carter de soufflante

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3318554A (en) * 1964-09-22 1967-05-09 Rolls Royce Mounting arrangement for engines
GB1318748A (en) * 1970-08-11 1973-05-31 Secr Defence Gas turgine ducted fan engines for aircraft
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
SU849694A1 (ru) * 1980-03-12 1996-09-20 А.А. Бобух Устройство для крепления двухконтурного турбореактивного двигателя
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine
FR2661213B1 (fr) * 1990-04-19 1992-07-03 Snecma Moteur d'aviation a tres grand taux de dilution et du type dit contrafan avant.
US5524847A (en) * 1993-09-07 1996-06-11 United Technologies Corporation Nacelle and mounting arrangement for an aircraft engine
FR2730275B1 (fr) * 1995-02-03 1997-03-28 Aerospatiale Dispositif d'etancheite entre une entree d'air et un carter de soufflante de turboreacteur a double flux
FR2732074B1 (fr) * 1995-03-21 1997-06-06 Aerospatiale Turboreacteur a double flux a nacelle flottante
GB9602130D0 (en) * 1996-02-02 1996-04-03 Rolls Royce Plc Improved method of combining ducted fan gas turbine engine modules and aircraft structure
US6659878B2 (en) * 2001-03-30 2003-12-09 General Electric Company Method and apparatus for coupling male threads to female threads
GB2375513B (en) * 2001-05-19 2005-03-23 Rolls Royce Plc A mounting arrangement for a gas turbine engine
US6652222B1 (en) * 2002-09-03 2003-11-25 Pratt & Whitney Canada Corp. Fan case design with metal foam between Kevlar
FR2851226B1 (fr) * 2003-02-19 2005-05-20 Snecma Moteurs Structure porteuse pour un turbopropulseur et ensemble comportant une telle structure porteuse
US7090165B2 (en) * 2003-06-02 2006-08-15 Rolls-Royce Plc Aeroengine nacelle
FR2861364B1 (fr) * 2003-10-22 2006-02-03 Airbus France Dispositif de montage d'un carenage dispose entre une entree d'air d'un moteur d'aeronef et un mat.
WO2006059978A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Cantilevered tip turbine engine
GB0608983D0 (en) * 2006-05-06 2006-06-14 Rolls Royce Plc Aeroengine mount

Also Published As

Publication number Publication date
RU2391260C1 (ru) 2010-06-10
CA2653067C (fr) 2013-12-17
CN101472797B (zh) 2011-07-06
FR2902406B1 (fr) 2008-07-18
CN101472797A (zh) 2009-07-01
EP2029429A2 (de) 2009-03-04
ATE444896T1 (de) 2009-10-15
WO2007147965A2 (fr) 2007-12-27
EP2029429B1 (de) 2009-10-07
BRPI0712635A2 (pt) 2012-05-29
US8366039B2 (en) 2013-02-05
FR2902406A1 (fr) 2007-12-21
WO2007147965A3 (fr) 2008-02-14
CA2653067A1 (fr) 2007-12-27
JP2009541115A (ja) 2009-11-26
JP5097772B2 (ja) 2012-12-12
US20100176250A1 (en) 2010-07-15

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