CN101233047A - 航空器发动机的支架的改进主结构 - Google Patents

航空器发动机的支架的改进主结构 Download PDF

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Publication number
CN101233047A
CN101233047A CNA2006800280805A CN200680028080A CN101233047A CN 101233047 A CN101233047 A CN 101233047A CN A2006800280805 A CNA2006800280805 A CN A2006800280805A CN 200680028080 A CN200680028080 A CN 200680028080A CN 101233047 A CN101233047 A CN 101233047A
Authority
CN
China
Prior art keywords
bracket
main structure
composite
aircraft engine
engine according
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.)
Pending
Application number
CNA2006800280805A
Other languages
English (en)
Chinese (zh)
Inventor
O·夏娃
让-皮埃尔·卡巴纳克
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 CN101233047A publication Critical patent/CN101233047A/zh
Pending legal-status Critical Current

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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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Body Structure For Vehicles (AREA)
CNA2006800280805A 2005-08-05 2006-07-13 航空器发动机的支架的改进主结构 Pending CN101233047A (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0552439 2005-08-05
FR0552439A FR2889505B1 (fr) 2005-08-05 2005-08-05 Structure primaire de mat de moteur d'aeronef perfectionnee

Publications (1)

Publication Number Publication Date
CN101233047A true CN101233047A (zh) 2008-07-30

Family

ID=36177705

Family Applications (1)

Application Number Title Priority Date Filing Date
CNA2006800280805A Pending CN101233047A (zh) 2005-08-05 2006-07-13 航空器发动机的支架的改进主结构

Country Status (9)

Country Link
US (1) US20090294579A1 (enExample)
EP (1) EP1910166A1 (enExample)
JP (1) JP2009502642A (enExample)
CN (1) CN101233047A (enExample)
BR (1) BRPI0614230A2 (enExample)
CA (1) CA2616068A1 (enExample)
FR (1) FR2889505B1 (enExample)
RU (1) RU2008108513A (enExample)
WO (1) WO2007017339A1 (enExample)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103569367A (zh) * 2013-11-13 2014-02-12 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
CN106585999A (zh) * 2015-10-16 2017-04-26 空中客车运营简化股份公司 飞行器发动机挂架
WO2019105219A1 (zh) * 2017-11-30 2019-06-06 中国商用飞机有限责任公司 飞机发动机吊挂及其吊挂盒段

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE602006018362D1 (de) * 2006-01-11 2010-12-30 Boeing Co Aus verbundplatten und metallplatten zusammengesetzte flugzeugtragfläche
US8205825B2 (en) * 2008-02-27 2012-06-26 Spirit Aerosystems, Inc. Engine pylon made from composite material
FR2929245B1 (fr) * 2008-03-28 2010-05-14 Aircelle Sa Structure primaire d'un mat d'accrochage.
FR3032180B1 (fr) * 2015-01-30 2018-05-18 Airbus Operations Ensemble propulsif comportant un turboreacteur et un mat d'accrochage permettant une nouvelle distribution des efforts entre le turboreacteur et la voilure
FR3052745B1 (fr) 2016-06-15 2018-05-25 Airbus Operations Mat d'aeronef comprenant au moins un cadre lateral en forme de treillis et aeronef comprenant ledit mat
FR3072945B1 (fr) * 2017-10-27 2020-11-20 Airbus Operations Sas Structure primaire de mat de support d'un groupe propulseur d'aeronef comportant une partie inferieure en u obtenue de maniere monobloc ou par soudage
FR3072946A1 (fr) * 2017-10-27 2019-05-03 Airbus Operations Structure primaire de mat de support d'un groupe propulseur d'aeronef en caisson formee par assemblage de deux demi-coquilles
FR3087188B1 (fr) * 2018-10-12 2021-05-21 Airbus Operations Sas Panneau structural raidi pour aeronef, presentant une conception amelioree

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US4437627A (en) * 1982-03-12 1984-03-20 The Boeing Company Integrated power plant installation system
US4471609A (en) * 1982-08-23 1984-09-18 The Boeing Company Apparatus and method for minimizing engine backbone bending
US4539253A (en) * 1984-03-30 1985-09-03 American Cyanamid Co. High impact strength fiber resin matrix composites
US5054715A (en) * 1988-11-10 1991-10-08 The Boeing Company Apparatus and methods for reducing aircraft lifting surface flutter
DE4234038C2 (de) * 1992-10-09 1997-07-03 Daimler Benz Aerospace Airbus Schalenbauteil aus Faserverbundwerkstoff
FR2698068B1 (fr) * 1992-11-16 1995-02-03 Airbus Ind Avion et autre aéronef à moteur pourvu d'ailes.
JPH0776051A (ja) * 1993-06-18 1995-03-20 Toray Ind Inc Ｆｒｐ製パネル及びその製造方法
US5467941A (en) * 1993-12-30 1995-11-21 The Boeing Company Pylon and engine installation for ultra-high by-pass turbo-fan engines
JP2954836B2 (ja) * 1994-09-14 1999-09-27 川崎重工業株式会社 繊維強化樹脂系型材の成形方法
DE69529453T2 (de) * 1994-12-26 2003-10-02 Honda Giken Kogyo K.K., Tokio/Tokyo Mehrschichtige Platte aus faserverstärktem Kunststoff, und stossdämpfende Struktur
JPH11104965A (ja) * 1997-09-30 1999-04-20 Noritake Co Ltd 高速研削用砥石
JP2000142488A (ja) * 1998-11-13 2000-05-23 Toray Ind Inc トラックの荷台フロア
JP3861664B2 (ja) * 2001-11-14 2006-12-20 東レ株式会社 Ｆｒｐ製パネル同士の接合構造
JPWO2004085856A1 (ja) * 2003-03-25 2006-06-29 株式会社日立メディコ 流体圧式アクチュエータ及びそれを用いた持続的他動運動装置
JP2004338465A (ja) * 2003-05-14 2004-12-02 Murata Mach Ltd コーナーフィーラー及びコーナーフィーラーを充填した構造体及びコーナーフィーラーの製造方法
US7083143B2 (en) * 2003-10-17 2006-08-01 The Boeing Company Apparatuses and methods for attaching engines and other structures to aircraft wings
FR2891251B1 (fr) * 2005-09-28 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891803B1 (fr) * 2005-10-07 2007-11-30 Airbus France Sas Structure rigide pour mat d'accrochage de moteur d'aeronef, et mat comportant une telle structure
US8205825B2 (en) * 2008-02-27 2012-06-26 Spirit Aerosystems, Inc. Engine pylon made from composite material

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103569367A (zh) * 2013-11-13 2014-02-12 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
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
CN106585999A (zh) * 2015-10-16 2017-04-26 空中客车运营简化股份公司 飞行器发动机挂架
CN106585999B (zh) * 2015-10-16 2021-12-14 空中客车运营简化股份公司 飞行器发动机挂架
WO2019105219A1 (zh) * 2017-11-30 2019-06-06 中国商用飞机有限责任公司 飞机发动机吊挂及其吊挂盒段

Also Published As

Publication number Publication date
US20090294579A1 (en) 2009-12-03
FR2889505A1 (fr) 2007-02-09
BRPI0614230A2 (pt) 2012-12-11
EP1910166A1 (fr) 2008-04-16
RU2008108513A (ru) 2009-09-10
WO2007017339A1 (fr) 2007-02-15
JP2009502642A (ja) 2009-01-29
FR2889505B1 (fr) 2007-09-14
CA2616068A1 (fr) 2007-02-15

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Legal Events

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C53 Correction of patent of invention or patent application
CB02 Change of applicant information

Address after: France Toulouse

Applicant after: Airbus Operations S.A.S.

Address before: France Toulouse

Applicant before: Airbus France

Address after: France Toulouse

Applicant after: AIRBUS FRANCE

Address before: France Toulouse

Applicant before: Airbus France

COR Change of bibliographic data

Free format text: CORRECT: APPLICANT; FROM: AIRBUS FRANCE TO: AIRBUS OPERATIONS GMBH

C12 Rejection of a patent application after its publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20080730