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DE602007006510D1 - Flügelummantelungsplattenanordnung und flügelummantelungsplatte für einen flugzeugflügel und herstellungsverfahren dafür - Google Patents

Flügelummantelungsplattenanordnung und flügelummantelungsplatte für einen flugzeugflügel und herstellungsverfahren dafür

Info

Publication number
DE602007006510D1
DE602007006510D1 DE602007006510T DE602007006510T DE602007006510D1 DE 602007006510 D1 DE602007006510 D1 DE 602007006510D1 DE 602007006510 T DE602007006510 T DE 602007006510T DE 602007006510 T DE602007006510 T DE 602007006510T DE 602007006510 D1 DE602007006510 D1 DE 602007006510D1
Authority
DE
Germany
Prior art keywords
wing
mounting plate
manufacturing
method therefor
plane
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.)
Active
Application number
DE602007006510T
Other languages
English (en)
Inventor
Michael Tucker
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 Ltd
Original Assignee
Airbus UK 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 UK Ltd filed Critical Airbus UK Ltd
Publication of DE602007006510D1 publication Critical patent/DE602007006510D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Connection Of Plates (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Casting Support Devices, Ladles, And Melt Control Thereby (AREA)
  • Diaphragms For Electromechanical Transducers (AREA)
  • Toys (AREA)
  • Air Bags (AREA)
DE602007006510T 2006-07-13 2007-07-05 Flügelummantelungsplattenanordnung und flügelummantelungsplatte für einen flugzeugflügel und herstellungsverfahren dafür Active DE602007006510D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0613949.7A GB0613949D0 (en) 2006-07-13 2006-07-13 A wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof
PCT/GB2007/050382 WO2008007135A2 (en) 2006-07-13 2007-07-05 A wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof

Publications (1)

Publication Number Publication Date
DE602007006510D1 true DE602007006510D1 (de) 2010-06-24

Family

ID=36955605

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007006510T Active DE602007006510D1 (de) 2006-07-13 2007-07-05 Flügelummantelungsplattenanordnung und flügelummantelungsplatte für einen flugzeugflügel und herstellungsverfahren dafür

Country Status (11)

Country Link
US (1) US8398024B2 (de)
EP (1) EP2054297B1 (de)
JP (1) JP2009542524A (de)
CN (1) CN101432191B (de)
AT (1) ATE467554T1 (de)
BR (1) BRPI0712214A2 (de)
CA (1) CA2644269C (de)
DE (1) DE602007006510D1 (de)
GB (1) GB0613949D0 (de)
RU (1) RU2438925C2 (de)
WO (1) WO2008007135A2 (de)

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US8100316B2 (en) * 2008-05-29 2012-01-24 Airbus Operations Gmbh Method for joining aircraft fuselage elements by friction stir welding (fsw)
US7857191B2 (en) * 2008-06-16 2010-12-28 Embraer-Empresa Brasileira De Aeronautica S.A. Friction stir welding (FSW) methods and systems and friction stir welded components made thereby
KR101649376B1 (ko) * 2008-10-13 2016-08-31 한국전자통신연구원 Ｍｄｃｔ 기반 음성/오디오 통합 부호화기의 ｌｐｃ 잔차신호 부호화/복호화 장치
GB201000878D0 (en) * 2010-01-20 2010-03-10 Airbus Operations Ltd Sandwich panel
GB201018185D0 (en) * 2010-10-28 2010-12-08 Airbus Operations Ltd Wing tip device attachment apparatus and method
ES2402463B1 (es) * 2010-11-30 2014-03-13 Airbus Operations, S.L. Un revestimiento de una superficie sustentadora de una aeronave.
CN102139759A (zh) * 2011-02-17 2011-08-03 中国航空工业集团公司西安飞机设计研究所 一种大尺寸复合材料整体壁板补强方法
US9168998B2 (en) * 2011-11-23 2015-10-27 The Boeing Company Composite propeller spar
CN102806617B (zh) * 2012-06-04 2014-11-05 中航复合材料有限责任公司 一种整体成型“工”型加筋复合材料壁板的模具
CN102848498B (zh) * 2012-06-04 2014-08-13 中航复合材料有限责任公司 一种整体成型“j”型加筋复合材料壁板的模具
FR2995236B1 (fr) * 2012-09-07 2015-05-01 Airbus Operations Sas Procede et systeme ameliores de soudage par friction malaxage d'un raidisseur sur un panneau d'aeronef.
FR2995237B1 (fr) 2012-09-07 2015-05-01 Airbus Operations Sas Systeme ameliore de soudage par friction malaxage comprenant un contre-appui mobile.
GB201220937D0 (en) * 2012-11-21 2013-01-02 Airbus Uk Ltd Modular structural assembly
JP5840161B2 (ja) * 2013-03-04 2016-01-06 本田技研工業株式会社 異種材接合体の接合方法
US9341207B2 (en) * 2013-07-30 2016-05-17 Gulfstream Aerospace Corporation Web component and method of making a web component
US9676549B2 (en) * 2014-12-02 2017-06-13 Fontaine Commercial Trailer, Inc. Floor assembly for transportable refrigerated container
CN105235237A (zh) * 2015-11-18 2016-01-13 江西洪都航空工业集团有限责任公司 一种复合材料j型加筋壁板成型工艺及成型工装
CN105346102B (zh) * 2015-11-27 2018-02-23 沈阳飞机工业（集团）有限公司 复合材料j型纵墙定位整体成型工装及其成型方法
US10696373B2 (en) * 2016-09-13 2020-06-30 The Boeing Company Aircraft wings and aircraft including such aircraft wings
CN108100230A (zh) * 2017-12-01 2018-06-01 中国直升机设计研究所 一种直升机平尾翼盒
JP2019131071A (ja) * 2018-01-31 2019-08-08 三菱重工業株式会社 航空機
US11214353B2 (en) * 2018-06-01 2022-01-04 Airbus Operations Gmbh Wing arrangement for an aircraft and aircraft
CN108688793B (zh) * 2018-07-27 2023-11-24 中国工程物理研究院总体工程研究所 筒式发射无人机机翼折叠展开机构
FR3089442B1 (fr) * 2018-12-05 2020-12-18 Airbus Operations Sas Procédé d’assemblage d’au moins deux pièces par soudage par transparence, procédé d’assemblage d’une structure primaire d’un mât d’aéronef par soudage par transparence, structure primaire d’un mât d’aéronef ainsi obtenue et aéronef comprenant ladite structure primaire
CN109624355A (zh) * 2018-12-10 2019-04-16 西安航空职业技术学院 高性能vari工艺成型复合材料的出胶结构及方法
NL2023459B1 (en) * 2019-07-08 2021-02-02 Kok & Van Engelen Composite Structures B V Fuselage structure of an aircraft and method for manufacturing the same
US11701737B2 (en) * 2019-09-10 2023-07-18 Qingdao Cimc Reefer Trailer Co., Ltd. Friction-stir-welded sheet-and-post sidewall
US11498656B1 (en) * 2021-04-26 2022-11-15 Rohr, Inc. Airfoil system with embedded electric device

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JPS5014319Y1 (de) * 1967-08-29 1975-05-02
US3827661A (en) * 1972-07-26 1974-08-06 Ryson Aviat Corp Aircraft wing structure and method of assembly
SU458177A1 (ru) * 1973-04-03 1991-10-30 Предприятие П/Я В-2739 Узел соединени деталей конструкций из композиционного материала слоистой структуры с волокнистым наполнителем
CA1010002A (en) 1973-04-25 1977-05-10 Minnesota Mining And Manufacturing Company Guide roller biasing shim liner
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Also Published As

Publication number Publication date
CN101432191B (zh) 2012-03-07
RU2008149090A (ru) 2010-08-20
ATE467554T1 (de) 2010-05-15
US8398024B2 (en) 2013-03-19
GB0613949D0 (en) 2006-08-23
BRPI0712214A2 (pt) 2012-03-13
US20090200423A1 (en) 2009-08-13
CA2644269A1 (en) 2008-01-17
EP2054297A2 (de) 2009-05-06
JP2009542524A (ja) 2009-12-03
CN101432191A (zh) 2009-05-13
WO2008007135A3 (en) 2008-05-22
EP2054297B1 (de) 2010-05-12
CA2644269C (en) 2015-03-24
RU2438925C2 (ru) 2012-01-10
WO2008007135A2 (en) 2008-01-17

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