JP2009519861A - 航空機構造に使用される継手 - Google Patents

航空機構造に使用される継手 Download PDF

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Publication number
JP2009519861A
JP2009519861A JP2008546567A JP2008546567A JP2009519861A JP 2009519861 A JP2009519861 A JP 2009519861A JP 2008546567 A JP2008546567 A JP 2008546567A JP 2008546567 A JP2008546567 A JP 2008546567A JP 2009519861 A JP2009519861 A JP 2009519861A
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JP
Japan
Prior art keywords
joint
plate
aircraft structure
skin
structure 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
JP2008546567A
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English (en)
Japanese (ja)
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JP2009519861A5 (enExample
Inventor
クーパー、ポール、アンソニー
Original Assignee
エアバス・ユ―ケ―・リミテッド
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.)
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Application filed by エアバス・ユ―ケ―・リミテッド filed Critical エアバス・ユ―ケ―・リミテッド
Publication of JP2009519861A publication Critical patent/JP2009519861A/ja
Publication of JP2009519861A5 publication Critical patent/JP2009519861A5/ja
Pending legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Adhesives Or Adhesive Processes (AREA)
  • Road Paving Structures (AREA)
JP2008546567A 2005-12-20 2006-11-28 航空機構造に使用される継手 Pending JP2009519861A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0525896.7A GB0525896D0 (en) 2005-12-20 2005-12-20 A joint for use in aircraft construction
PCT/GB2006/004439 WO2007071905A1 (en) 2005-12-20 2006-11-28 A joint for use in aircraft construction

Publications (2)

Publication Number Publication Date
JP2009519861A true JP2009519861A (ja) 2009-05-21
JP2009519861A5 JP2009519861A5 (enExample) 2010-01-07

Family

ID=35840772

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008546567A Pending JP2009519861A (ja) 2005-12-20 2006-11-28 航空機構造に使用される継手

Country Status (11)

Country Link
US (2) USRE47738E1 (enExample)
EP (1) EP1963178B1 (enExample)
JP (1) JP2009519861A (enExample)
CN (1) CN101341070A (enExample)
AT (1) ATE476359T1 (enExample)
BR (1) BRPI0620070A2 (enExample)
CA (1) CA2633106C (enExample)
DE (1) DE602006016006D1 (enExample)
GB (1) GB0525896D0 (enExample)
RU (1) RU2427500C2 (enExample)
WO (1) WO2007071905A1 (enExample)

Cited By (3)

* Cited by examiner, † Cited by third party
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JP2011515278A (ja) * 2008-03-25 2011-05-19 エアバス オペレーションズ リミティド 航空機用の複合材継手
JP2012530653A (ja) * 2009-06-22 2012-12-06 ザ・ボーイング・カンパニー 空気流を改善した外板パネルジョイント
JP2016175631A (ja) * 2014-09-17 2016-10-06 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 航空機翼の複合固定縁及びその取り付け方法

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FR2916424B1 (fr) * 2007-05-23 2009-08-21 Airbus France Sa Mat d'accrochage de moteur pour aeronef comprenant une cale biaise pour la fixation de l'attache moteur avant
RU2476348C2 (ru) * 2007-05-31 2013-02-27 Эйрбас Оператионс Гмбх Способ производства составной обшивки в области авиационной и космической промышленности
US8398027B2 (en) * 2007-09-17 2013-03-19 The Boeing Company Method and apparatus for reinforcing composite structures
US8490920B2 (en) * 2007-10-12 2013-07-23 Abe Karem Composite bulkhead and skin construction
DE102008013365B4 (de) * 2008-03-10 2011-03-17 Airbus Operations Gmbh Querstoßverbindung zwischen zwei Rumpfsektionen
GB0805963D0 (en) * 2008-04-02 2008-05-07 Airbus Uk Ltd Aircraft structure
IT1390909B1 (it) * 2008-07-16 2011-10-19 Alenia Aeronautica Spa Elemento strutturale a rigidezza calcolata, con caratteristiche di assorbimento di spostamenti e copertura interstizi
FR2936495B1 (fr) * 2008-09-30 2011-06-03 Airbus France Assemblage de panneaux pour fuselage d'aeronef.
GB0901640D0 (en) * 2009-02-03 2009-03-11 Airbus Uk Ltd Joint
ES2384920B1 (es) * 2009-03-31 2013-05-21 Airbus Operations, S.L. Pieza de material con una rampa entre dos zonas.
GB0905818D0 (en) * 2009-04-06 2009-05-20 Airbus Uk Ltd Coupling assembly
GB0910938D0 (en) * 2009-06-25 2009-08-05 Airbus Operations Ltd Method of manufacturing a structure
EP2316629B1 (en) * 2009-10-27 2012-05-23 Lm Glasfiber A/S Modular mould system for manufacturing a shell part
DE102009060693A1 (de) * 2009-12-29 2011-06-30 Airbus Operations GmbH, 21129 Versteifungselement für ein Luftfahrzeug und Flächengebilde mit einem derartigen Versteifungselement
ES2396327B1 (es) * 2010-06-10 2014-02-06 Airbus Operations, S.L. Procedimiento para la fabricación de piezas grandes de material compuesto controlando el espesor de sus bordes
DE102010026839A1 (de) 2010-07-12 2012-01-12 Airbus Operations Gmbh Aerodynamische Verkleidungsvorrichtung, Flugzeug-Bauteilanordnung mit einer aerodynamischen Verkleidungsvorrichtung sowie Verfahren zur Montage eines solchen Verkleidungsteils
US8333345B2 (en) * 2010-08-26 2012-12-18 The Boeing Company Composite aircraft joint
GB201016279D0 (en) 2010-09-28 2010-11-10 Airbus Operations Ltd Stiffener run-out
ES2396881B1 (es) * 2010-11-30 2014-01-29 Airbus Operations, S.L. Disposición de interfaz entre dos componentes de una estructura de una aeronave usando una pieza de sellado.
ES2396882B1 (es) * 2010-11-30 2014-01-29 Airbus Operations, S.L. Disposición de interfaz entre dos componentes de una estructura de una aeronave.
ES2403361B1 (es) * 2010-12-17 2014-04-29 Airbus Operations, S.L. Optimización de estructuras sometidas a corrientes de gases calientes.
FR2970463B1 (fr) * 2011-01-17 2013-02-15 Airbus Operations Sas Dispositif d'eclissage a tenue mecanique amelioree.
RU2475425C1 (ru) * 2011-10-06 2013-02-20 Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" Устройство металлизации корпуса изделия
US20130114994A1 (en) 2011-11-04 2013-05-09 Robert Erik Grip Truss end pad fitting
US9574587B2 (en) 2011-11-04 2017-02-21 The Boeing Company Preloading a fastener of a mechanical fitting
GB201200912D0 (en) * 2012-01-19 2012-02-29 Airbus Operations Ltd Fastener receptacle strip
GB201205079D0 (en) * 2012-03-22 2012-05-09 Airbus Operations Ltd Seal assembly for an aircraft wing
US9180956B1 (en) * 2012-04-11 2015-11-10 The Boeing Company Methods and apparatus for attaching an aircraft wing assembly to an aircraft body
ES2426111B1 (es) * 2012-04-17 2015-03-24 Airbus Operations S.L. Interfaz para superficie de sustentación de aeronave
EP2653376B1 (en) * 2012-04-18 2016-03-23 Airbus Operations, S.L. Bolted joint of the cover of an access opening in an aircraft lifting surface
GB201209437D0 (en) * 2012-05-28 2012-07-11 Kitchener Renato Power supply and battery charger
US8985514B2 (en) * 2012-06-20 2015-03-24 The Boeing Company Composite structural panels and aircraft fuselages
US8857765B2 (en) * 2012-10-16 2014-10-14 The Boeing Company Method and apparatus for attaching an aircraft fuselage frame to a wing box
EP2909486B1 (en) * 2012-10-22 2018-12-12 BAE SYSTEMS plc Hybrid joint manufacutring
US9415853B2 (en) * 2013-01-30 2016-08-16 The Boeing Company Surface sealing system
FR3015433B1 (fr) 2013-12-23 2016-02-12 Airbus Operations Sas Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage
US9399507B2 (en) 2014-01-22 2016-07-26 The Boeing Company Joints between a composite skin and a load-bearing component and methods of forming same
US9676469B2 (en) 2014-04-10 2017-06-13 Lockheed Martin Corporation System and method for fastening structures
US10603888B2 (en) * 2014-04-10 2020-03-31 The Boeing Company Filling and leveling methods and apparatus for building tight tolerance surfaces
US9896190B1 (en) * 2014-05-07 2018-02-20 The Boeing Company Wing leading edge architecture suitable for laminar flow
EP3142923B1 (en) * 2014-05-15 2020-05-06 Sikorsky Aircraft Corporation Metallic dimpled doubler
US9925625B2 (en) * 2015-05-04 2018-03-27 The Boeing Company Assembly of an aircraft structure assembly without shimming, locating fixtures or final-hole-size drill jigs
DE102016210325B4 (de) * 2016-06-10 2021-07-15 Airbus Operations Gmbh Bauteilanordnung zur Ausbildung einer Tragstruktur eines Luft- oder Raumfahrzeugs
CN106697327B (zh) * 2016-12-19 2019-10-18 中航成飞民用飞机有限责任公司 飞机壁板对接结构
US10773789B2 (en) * 2017-07-07 2020-09-15 The Boeing Company Skin-panel interface of an aircraft
CN109677586A (zh) * 2019-01-18 2019-04-26 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种腹板、飞机机翼和飞机
US11884055B2 (en) * 2019-03-26 2024-01-30 The Boeing Company Laminated hybrid metallized polymer films, system, and method for erosion protection of composite structures
US11383820B2 (en) * 2019-06-11 2022-07-12 The Boeing Company Aerodynamic surface lap splice
CN110466734B (zh) * 2019-08-26 2022-08-19 中国航空工业集团公司沈阳飞机设计研究所 一种锯齿缝对接蒙皮的带板
US11524762B2 (en) * 2020-02-21 2022-12-13 The Boeing Company Fuselage structure splice
US11572152B2 (en) 2020-05-21 2023-02-07 The Boeing Company Structural composite airfoils with a single spar, and related methods
US11401026B2 (en) 2020-05-21 2022-08-02 The Boeing Company Structural composite airfoils with a single spar, and related methods
US11554848B2 (en) 2020-05-21 2023-01-17 The Boeing Company Structural composite airfoils with a single spar, and related methods
US11453476B2 (en) * 2020-05-21 2022-09-27 The Boeing Company Structural composite airfoils with an improved leading edge, and related methods
CN114771802A (zh) 2021-01-22 2022-07-22 波音公司 空气动力学结构以及形成空气动力学结构的方法
EP4053014B1 (en) * 2021-03-05 2024-12-18 The Boeing Company Assembly and method connecting an aircraft wing aft spar root to an aircraft body fuselage
CN113376044B (zh) * 2021-06-10 2022-07-12 中国兵器工业第五九研究所 一种高温高压气体冲刷实验装置
CN114684346A (zh) * 2021-12-31 2022-07-01 中国航空工业集团公司西安飞机设计研究所 一种长桁接头
EP4303120A1 (en) * 2022-07-07 2024-01-10 Airbus Operations S.L.U. Composite multi-spar aircraft lifting surface
CN119489923A (zh) * 2024-12-25 2025-02-21 中国航空工业集团公司西安飞机设计研究所 一种加筋壁板对接结构及设计方法

Citations (3)

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DE704327C (de) * 1939-02-09 1941-03-28 Henschel Flugzeug Werke A G Flugzeugfluegel
JPS63240494A (ja) * 1987-03-26 1988-10-06 川崎重工業株式会社 航空機用翼の前縁保護構造
US20050213278A1 (en) * 2004-03-23 2005-09-29 Hawley Arthur V Lightning damage protection for composite aircraft

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DE704327C (de) * 1939-02-09 1941-03-28 Henschel Flugzeug Werke A G Flugzeugfluegel
JPS63240494A (ja) * 1987-03-26 1988-10-06 川崎重工業株式会社 航空機用翼の前縁保護構造
US20050213278A1 (en) * 2004-03-23 2005-09-29 Hawley Arthur V Lightning damage protection for composite aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011515278A (ja) * 2008-03-25 2011-05-19 エアバス オペレーションズ リミティド 航空機用の複合材継手
JP2012530653A (ja) * 2009-06-22 2012-12-06 ザ・ボーイング・カンパニー 空気流を改善した外板パネルジョイント
JP2016175631A (ja) * 2014-09-17 2016-10-06 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 航空機翼の複合固定縁及びその取り付け方法

Also Published As

Publication number Publication date
ATE476359T1 (de) 2010-08-15
GB0525896D0 (en) 2006-02-01
EP1963178A1 (en) 2008-09-03
RU2427500C2 (ru) 2011-08-27
US20080258008A1 (en) 2008-10-23
CN101341070A (zh) 2009-01-07
DE602006016006D1 (de) 2010-09-16
CA2633106C (en) 2013-08-06
BRPI0620070A2 (pt) 2011-11-01
USRE47738E1 (en) 2019-11-26
EP1963178B1 (en) 2010-08-04
RU2008129606A (ru) 2010-01-27
US7909290B2 (en) 2011-03-22
CA2633106A1 (en) 2007-06-28
WO2007071905A1 (en) 2007-06-28

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