ATE476359T1 - Verbindung zur verwendung in einer flugzeugkonstruktion - Google Patents

Verbindung zur verwendung in einer flugzeugkonstruktion

Info

Publication number
ATE476359T1
ATE476359T1 AT06808699T AT06808699T ATE476359T1 AT E476359 T1 ATE476359 T1 AT E476359T1 AT 06808699 T AT06808699 T AT 06808699T AT 06808699 T AT06808699 T AT 06808699T AT E476359 T1 ATE476359 T1 AT E476359T1
Authority
AT
Austria
Prior art keywords
butt
strap
skin
exterior surface
exterior
Prior art date
Application number
AT06808699T
Other languages
German (de)
English (en)
Inventor
Paul Cooper
Original Assignee
Airbus Operations Ltd
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 Ltd filed Critical Airbus Operations Ltd
Application granted granted Critical
Publication of ATE476359T1 publication Critical patent/ATE476359T1/de

Links

Classifications

    • 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)
AT06808699T 2005-12-20 2006-11-28 Verbindung zur verwendung in einer flugzeugkonstruktion ATE476359T1 (de)

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 (1)

Publication Number Publication Date
ATE476359T1 true ATE476359T1 (de) 2010-08-15

Family

ID=35840772

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06808699T ATE476359T1 (de) 2005-12-20 2006-11-28 Verbindung zur verwendung in einer flugzeugkonstruktion

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)

Families Citing this family (65)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0609166D0 (en) * 2006-05-09 2006-06-21 Airbus Uk Ltd Apparatus for and method of inhibiting delamination
JP4657194B2 (ja) * 2006-11-20 2011-03-23 本田技研工業株式会社 前縁スキンの段差調整構造および前縁スキンの組付方法
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
GB0805268D0 (en) * 2008-03-25 2008-04-30 Airbus Uk Ltd Composite joint protection
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
US8282042B2 (en) * 2009-06-22 2012-10-09 The Boeing Company Skin panel joint for improved airflow
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
US10329009B2 (en) * 2014-09-17 2019-06-25 The Boeing Company Composite wing edge attachment and method
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

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE704327C (de) * 1939-02-09 1941-03-28 Henschel Flugzeug Werke A G Flugzeugfluegel
GB1022131A (en) * 1963-06-10 1966-03-09 Monte Copter Inc Sectional airfoil
IL63240A (en) 1980-07-11 1984-12-31 Weecan Marine Method and apparatus for manufacturing an integral shell formed body
US4507011A (en) * 1982-05-03 1985-03-26 The Boeing Company Reinforced elastomer attachment joint
SU1420823A1 (ru) * 1987-01-30 1996-09-20 Е.А. Бычковский Хвостовая часть крыла самолета
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
US4888451A (en) 1988-11-29 1989-12-19 United Technologies Corporation Electrical continuity means for composite joints
US5803406A (en) * 1996-04-22 1998-09-08 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Integrated thermal insulation system for spacecraft
US6375120B1 (en) * 1997-07-14 2002-04-23 Jason M. Wolnek Method and apparatus for building a metal/composite hybrid airplane component
RU12819U1 (ru) * 1999-04-28 2000-02-10 Егер Владимир Сергеевич Композитное кессонное крыло легкого самолета
WO2002014147A1 (en) * 2000-08-11 2002-02-21 Dunlop Aerospace Limited Wheel hub assemblies
DE10238820A1 (de) * 2002-08-23 2004-03-11 Airbus Deutschland Gmbh Anordung zur Erfindung von dünnwandigen Metallstrukturen
GB0329373D0 (en) * 2003-12-18 2004-01-21 Airbus Uk Ltd Method of joining structural elements in an aircraft
US7554785B2 (en) * 2004-03-23 2009-06-30 The Boeing Company Lightning damage protection for composite aircraft
US20060251496A1 (en) * 2004-07-09 2006-11-09 Bae Systems Plc Fastener arrangement for fastening a detachable panel
US7296656B2 (en) * 2005-04-22 2007-11-20 United Technologies Corporation Acoustic mechanical retainer
FR2905739B1 (fr) * 2006-09-08 2008-11-07 Airbus France Sas Assemblage de panneaux et procede de montage d'un assemblage de panneaux
JP4657194B2 (ja) * 2006-11-20 2011-03-23 本田技研工業株式会社 前縁スキンの段差調整構造および前縁スキンの組付方法
US8016230B2 (en) * 2007-05-11 2011-09-13 The Boeing Company Fastner-free primary structural joint for sandwich panels
US8398027B2 (en) * 2007-09-17 2013-03-19 The Boeing Company Method and apparatus for reinforcing composite structures

Also Published As

Publication number Publication date
GB0525896D0 (en) 2006-02-01
JP2009519861A (ja) 2009-05-21
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

Similar Documents

Publication Publication Date Title
ATE476359T1 (de) Verbindung zur verwendung in einer flugzeugkonstruktion
USD752722S1 (en) Pipe cuff
WO2011100321A3 (en) Seal arrangements for ultrasonically powered surgical instruments
USD626169S1 (en) Sunglasses lanyard
WO2011133423A3 (en) Load sharing bone fastener and methods of use
USD735340S1 (en) Hearing aid
ATE465084T1 (de) Flugzeugstruktur
GB2474766B (en) Ceramic metallic interlocked components and methods of making and using the same
EA200700565A1 (ru) Подфюзеляжный обтекатель летательного аппарата
TWD137489S1 (zh) 硬管接頭段
JP2012501469A5 (enExample)
CR20110532A (es) Caja con paredes laterales plegables teniendo una estructura de pared lateral estable
BR0203556B1 (pt) aeronave com carenagem ventral e junta para esta.
PL1848648T3 (pl) Zespół uszczelniający dla pojemnika ciśnieniowego
WO2008113612A3 (en) Gap covering device
EP2333319A3 (en) A fluid turbine blade and method of providing the same
EP2184423A3 (de) Sockelleiste zum Abdecken eines Belagsrandes
CA122665S (en) Trigger latch
AU306659S (en) Two-way flashlight
EP2530251A3 (en) Hinge seal
AU313823S (en) Pizza scissors
TW200734215A (en) Opening portion structure
WO2011109513A3 (en) Dynamic vertebral construct
SE0501638L (sv) En fogprofil till en panel
EP2345532A3 (en) Oblong configuration for bonded patch

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties