BRPI0614230A2 - estrutura primária de estribo de motor de aeronave - Google Patents

estrutura primária de estribo de motor de aeronave Download PDF

Info

Publication number
BRPI0614230A2
BRPI0614230A2 BRPI0614230-3A BRPI0614230A BRPI0614230A2 BR PI0614230 A2 BRPI0614230 A2 BR PI0614230A2 BR PI0614230 A BRPI0614230 A BR PI0614230A BR PI0614230 A2 BRPI0614230 A2 BR PI0614230A2
Authority
BR
Brazil
Prior art keywords
panels
composite
stirrup
aircraft engine
primary structure
Prior art date
Application number
BRPI0614230-3A
Other languages
English (en)
Portuguese (pt)
Inventor
Olivier Eve
Jean-Pierre Cabanac
Original Assignee
Airbus France
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 France filed Critical Airbus France
Publication of BRPI0614230A2 publication Critical patent/BRPI0614230A2/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
    • B64D27/02—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)
BRPI0614230-3A 2005-08-05 2006-07-13 estrutura primária de estribo de motor de aeronave BRPI0614230A2 (pt)

Applications Claiming Priority (3)

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
PCT/EP2006/064240 WO2007017339A1 (fr) 2005-08-05 2006-07-13 Structure primaire de mât de moteur d'aéronef perfectionnée

Publications (1)

Publication Number Publication Date
BRPI0614230A2 true BRPI0614230A2 (pt) 2012-12-11

Family

ID=36177705

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0614230-3A BRPI0614230A2 (pt) 2005-08-05 2006-07-13 estrutura primária de estribo de motor de aeronave

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)

Families Citing this family (11)

* 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.
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
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
FR3042475B1 (fr) * 2015-10-16 2018-07-13 Airbus Operations (S.A.S.) Mat porteur de moteur d'aeronef
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
CN107963225B (zh) * 2017-11-30 2021-06-04 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
FR3087188B1 (fr) * 2018-10-12 2021-05-21 Airbus Operations Sas Panneau structural raidi pour aeronef, presentant une conception amelioree

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Also Published As

Publication number Publication date
US20090294579A1 (en) 2009-12-03
FR2889505A1 (fr) 2007-02-09
EP1910166A1 (fr) 2008-04-16
RU2008108513A (ru) 2009-09-10
WO2007017339A1 (fr) 2007-02-15
CN101233047A (zh) 2008-07-30
JP2009502642A (ja) 2009-01-29
FR2889505B1 (fr) 2007-09-14
CA2616068A1 (fr) 2007-02-15

Similar Documents

Publication Publication Date Title
CN103661956B (zh) 包括涡轮发动机支承弓形件的用于飞行器的侧向推进单元
RU2641026C2 (ru) Силовые кессонные конструкции и способы их получения
CN103269950B (zh) 飞机结构组件
CA2343590C (en) Leading edge of supporting surfaces of aircraft
CN101883717B (zh) 由飞机的两个机身部分和用于连接机舱室蒙皮的连接结构组成的布置结构
US9533768B2 (en) Aircraft engine mounting system
JP4951059B2 (ja) 航空機構成材
CN101668679B (zh) 飞行器的机翼-机身段
US8684309B2 (en) Bracket
CN102442433B (zh) 用于航空器发动机附连挂架的具有连接杆的结合有三个对齐的球窝接头的推动力吸收设备
US8177167B2 (en) Central section of aircraft with ventral or belly fairing capable of movement
CN101448697B (zh) 飞机机身结构及其制造方法
CN109878742B (zh) 用于飞行器的组件和飞行器
CN101142120A (zh) 安装在附件支柱与航空发动机之间的装配系统的发动机附件
BR102013027906A2 (pt) Emenda de circunferência para unir estruturas de carcaça
EP2727824A2 (en) Reinforced aircraft fuselage
CN103129739B (zh) 飞行器的发动机的悬挂支柱的后部空气动力整流罩
BRPI0614230A2 (pt) estrutura primária de estribo de motor de aeronave
BRPI0616143A2 (pt) estribo de afixação de motor para uma aeronave e processo de fabricação do mesmo
ES2685274T5 (es) Distribución de cargas puntuales en paneles de nido de abeja
ES2398287A1 (es) Fuselaje de aeronave resistente al impacto y tolerante al daño.
CA2755840A1 (en) Fuselage cell structure for an aircraft of hybrid construction
US20210101689A1 (en) Engine pylon for coupling a jet engine to a wing of an aircraft
CN103857591B (zh) 改进的前起落架箱
US8317130B1 (en) Landing gear mount

Legal Events

Date Code Title Description
B06G Technical and formal requirements: other requirements [chapter 6.7 patent gazette]

Free format text: SOLICITA-SE A REGULARIZACAO DA PROCURACAO, UMA VEZ QUE BASEADO NO ARTIGO 216 1O DA LPI, O DOCUMENTO DE PROCURACAO DEVE SER APRESENTADO NO ORIGINAL, TRASLADO OU FOTOCOPIA AUTENTICADA.

B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 10A 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 2385 DE 20-09-2016 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.