JP2009519861A5 - - Google Patents

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Publication number
JP2009519861A5
JP2009519861A5 JP2008546567A JP2008546567A JP2009519861A5 JP 2009519861 A5 JP2009519861 A5 JP 2009519861A5 JP 2008546567 A JP2008546567 A JP 2008546567A JP 2008546567 A JP2008546567 A JP 2008546567A JP 2009519861 A5 JP2009519861 A5 JP 2009519861A5
Authority
JP
Japan
Prior art keywords
joint
aircraft structure
plate
structure according
skin
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
Other languages
English (en)
Japanese (ja)
Other versions
JP2009519861A (ja
Filing date
Publication date
Priority claimed from GBGB0525896.7A external-priority patent/GB0525896D0/en
Application filed filed Critical
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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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 JP2009519861A (ja) 2009-05-21
JP2009519861A5 true 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)

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US8857765B2 (en) * 2012-10-16 2014-10-14 The Boeing Company Method and apparatus for attaching an aircraft fuselage frame to a wing box
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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
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US10603888B2 (en) * 2014-04-10 2020-03-31 The Boeing Company Filling and leveling methods and apparatus for building tight tolerance surfaces
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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
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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
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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
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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
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