CN100548803C8 - 航空器的涡轮喷气发动机支架 - Google Patents

航空器的涡轮喷气发动机支架

Info

Publication number
CN100548803C8
CN100548803C8 CN200680035522.9A CN200680035522A CN100548803C8 CN 100548803 C8 CN100548803 C8 CN 100548803C8 CN 200680035522 A CN200680035522 A CN 200680035522A CN 100548803 C8 CN100548803 C8 CN 100548803C8
Authority
CN
China
Prior art keywords
turbojet engine
case
bracket
engine mounts
aircraft turbojet
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.)
Expired - Fee Related
Application number
CN200680035522.9A
Other languages
English (en)
Other versions
CN100548803B8 (zh
CN101272952A (zh
CN100548803C (zh
Inventor
利昂内尔·迪奥维
让-米歇尔·塞陶特
劳伦特·拉丰
戴维·沙尔捷
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
法国空中客车公司
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 法国空中客车公司 filed Critical 法国空中客车公司
Publication of CN101272952A publication Critical patent/CN101272952A/zh
Application granted granted Critical
Publication of CN100548803C publication Critical patent/CN100548803C/zh
Publication of CN100548803B8 publication Critical patent/CN100548803B8/zh
Publication of CN100548803C8 publication Critical patent/CN100548803C8/zh
Expired - Fee Related 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
    • 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
    • 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
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Body Structure For Vehicles (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Assembled Shelves (AREA)
  • Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)
  • Connection Of Plates (AREA)

Abstract

本发明涉及种用于航空器的涡轮喷气发动机支架，该支架包括中心箱体(22)，该中心箱体由通过横向肋(23)连接在起的两个侧板的组装构成，所述支架还包括固定于该箱体(22)的前部且布置在该箱体每侧的两个侧箱体(24a)，每侧箱体具有后封闭框架(46a)。本发明的特征在于，构成该箱体(22)的肋(23)之装备有两个侧延伸件(52a)，这两个侧延伸件与所述肋(23)整体制成并且分别从两个侧板向箱体(22)之外突出，这两个延伸件(52a)分别固定安装于这两个侧箱体中每个的框架(46a)上。
CN200680035522.9A 2005-10-03 2006-06-29 航空器的涡轮喷气发动机支架 Expired - Fee Related CN100548803C8 (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0552989 2005-10-03
FR0552989A FR2891526B1 (fr) 2005-10-03 2005-10-03 Mat d'accrochage de turboreacteur pour aeronef
PCT/EP2006/066873 WO2007039556A1 (fr) 2005-10-03 2006-09-29 Mat d'accrochage de turboreacteur pour aeronef

Publications (4)

Publication Number Publication Date
CN101272952A CN101272952A (zh) 2008-09-24
CN100548803C CN100548803C (zh) 2009-10-14
CN100548803B8 CN100548803B8 (zh) 2018-06-29
CN100548803C8 true CN100548803C8 (zh) 2018-06-29

Family

ID=36577371

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200680035522.9A Expired - Fee Related CN100548803C8 (zh) 2005-10-03 2006-06-29 航空器的涡轮喷气发动机支架

Country Status (10)

Country Link
US (1) US8070093B2 (zh)
EP (1) EP1931567B8 (zh)
JP (1) JP4864975B2 (zh)
CN (1) CN100548803C8 (zh)
AT (1) ATE552173T1 (zh)
BR (1) BRPI0616578B1 (zh)
CA (1) CA2624457C (zh)
FR (1) FR2891526B1 (zh)
RU (1) RU2399558C9 (zh)
WO (1) WO2007039556A1 (zh)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1912567B1 (en) 2005-08-04 2012-12-26 Bayer HealthCare, LLC Small lancing device
FR2920198B1 (fr) 2007-08-20 2009-10-30 Aircelle Sa Structure pour inverseur de poussee
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
US8205825B2 (en) * 2008-02-27 2012-06-26 Spirit Aerosystems, Inc. Engine pylon made from composite material
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.
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.
FR2928347B1 (fr) * 2008-03-07 2010-06-25 Aircelle Sa Structure d'accrochage pour turboreacteur
US20140174056A1 (en) * 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
FR2936493A1 (fr) * 2008-10-01 2010-04-02 Aircelle Sa Mat adapte pour supporter un turboracteur d'aeronef et nacelle associee a un mat.
FR2954278B1 (fr) * 2009-12-18 2012-01-20 Aircelle 7303 Structure support pour inverseur de poussee notamment a grilles
FR2965548B1 (fr) * 2010-10-01 2012-10-19 Airbus Operations Sas Mat d'accrochage d'un moteur d'aeronef comprenant deux attaches voilure avant a pions de cisaillement orthogonaux
FR2981046B1 (fr) * 2011-10-06 2013-10-25 Aircelle Sa Ensemble propulsif d'aeronef
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
CA2918320C (en) 2013-07-26 2018-05-15 Mra Systems, Inc. Aircraft engine pylon
FR3012793B1 (fr) * 2013-11-05 2017-05-05 Airbus Operations Sas Ensemble pour aeronef comprenant une ferrure fixee sur la partie extrados d'un caisson de voilure, pour le montage d'un mat d'accrochage sur ce caisson de voilure
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
CN106414241B (zh) 2013-11-18 2019-03-01 洛德公司 涡轮螺旋桨发动机的附接系统和方法
FR3015434B1 (fr) * 2013-12-23 2017-12-08 Snecma Suspension de turbomachine
FR3040076B1 (fr) * 2015-08-13 2017-08-11 Airbus Operations Sas Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau
FR3065442B1 (fr) * 2017-04-25 2021-03-19 Airbus Operations Sas Ensemble moteur pour aeronef comprenant une attache moteur avant integree au caisson du mat d'accrochage
JP2019131071A (ja) * 2018-01-31 2019-08-08 三菱重工業株式会社 航空機
US10806087B2 (en) * 2018-05-21 2020-10-20 Deere & Company Fan support arm
FR3106126B1 (fr) * 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine
FR3129376A1 (fr) * 2021-11-19 2023-05-26 Airbus Operations Mat réacteur pour coupler un turboréacteur à une aile d’un aéronef

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1516980A (en) * 1974-12-24 1978-07-05 Rolls Royce Mounting ducted fan gas turbine engines on aircraft
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
US4206893A (en) * 1978-09-27 1980-06-10 The Boeing Company Seal closure for slot in engine mounting strut
SU849694A1 (ru) * 1980-03-12 1996-09-20 А.А. Бобух Устройство для крепления двухконтурного турбореактивного двигателя
RU2104228C1 (ru) * 1993-07-01 1998-02-10 Самарское государственное научно-производственное предприятие "Труд" Устройство для крепления авиационного двигателя к самолету
US6095456A (en) * 1996-12-23 2000-08-01 The Boeing Company Strut-wing interface having dual upper links
US6126110A (en) * 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon
FR2793768B1 (fr) * 1999-05-17 2001-09-07 Aerospatiale Airbus Dispositif de montage sur un mat d'un ensemble propulsif d'aeronef et mat adapte a ce dispositif
FR2862944B1 (fr) * 2003-12-01 2006-02-24 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef
US7104306B2 (en) * 2004-06-14 2006-09-12 The Boeing Company Cast unitized primary truss structure and method

Also Published As

Publication number Publication date
US20080315033A1 (en) 2008-12-25
WO2007039556A8 (fr) 2009-06-11
JP4864975B2 (ja) 2012-02-01
JP2009509847A (ja) 2009-03-12
US8070093B2 (en) 2011-12-06
CN101272952A (zh) 2008-09-24
EP1931567B8 (fr) 2018-08-08
CA2624457A1 (en) 2007-04-12
RU2399558C9 (ru) 2019-12-30
CA2624457C (en) 2013-09-24
EP1931567B1 (fr) 2012-04-04
FR2891526B1 (fr) 2007-11-02
RU2399558C2 (ru) 2010-09-20
WO2007039556A1 (fr) 2007-04-12
CN100548803C (zh) 2009-10-14
BRPI0616578B1 (pt) 2018-10-23
RU2008117402A (ru) 2009-11-10
FR2891526A1 (fr) 2007-04-06
BRPI0616578A2 (pt) 2012-12-25
EP1931567A1 (fr) 2008-06-18
ATE552173T1 (de) 2012-04-15
BRPI0616578A8 (pt) 2018-05-08

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C06 Publication
C10 Entry into substantive examination
C14 Grant of patent or utility model
ASS Succession or assignment of patent right

Owner name: AIRBUS OPERATIONS S.A.S.

Free format text: FORMER OWNER: AIRBUS FRANCE

Effective date: 20120116

C41 Transfer of patent application or patent right or utility model
CI03 Correction of invention patent
CF01 Termination of patent right due to non-payment of annual fee