JP2012523348A5 - - Google Patents

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Publication number
JP2012523348A5
JP2012523348A5 JP2012504081A JP2012504081A JP2012523348A5 JP 2012523348 A5 JP2012523348 A5 JP 2012523348A5 JP 2012504081 A JP2012504081 A JP 2012504081A JP 2012504081 A JP2012504081 A JP 2012504081A JP 2012523348 A5 JP2012523348 A5 JP 2012523348A5
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JP
Japan
Prior art keywords
spar
wing structure
cap
structure according
web
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.)
Granted
Application number
JP2012504081A
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English (en)
Japanese (ja)
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JP5901516B2 (ja
JP2012523348A (ja
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Publication date
Priority claimed from GBGB0906157.3A external-priority patent/GB0906157D0/en
Application filed filed Critical
Publication of JP2012523348A publication Critical patent/JP2012523348A/ja
Publication of JP2012523348A5 publication Critical patent/JP2012523348A5/ja
Application granted granted Critical
Publication of JP5901516B2 publication Critical patent/JP5901516B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2012504081A 2009-04-09 2010-03-31 改良型ウイング構造体 Expired - Fee Related JP5901516B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB0906157.3 2009-04-09
GBGB0906157.3A GB0906157D0 (en) 2009-04-09 2009-04-09 Improved wing structure
PCT/GB2010/050555 WO2010116170A2 (en) 2009-04-09 2010-03-31 Improved wing structure

Publications (3)

Publication Number Publication Date
JP2012523348A JP2012523348A (ja) 2012-10-04
JP2012523348A5 true JP2012523348A5 (enExample) 2013-04-25
JP5901516B2 JP5901516B2 (ja) 2016-04-13

Family

ID=40750359

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012504081A Expired - Fee Related JP5901516B2 (ja) 2009-04-09 2010-03-31 改良型ウイング構造体

Country Status (7)

Country Link
US (1) US8616499B2 (enExample)
EP (1) EP2417022B1 (enExample)
JP (1) JP5901516B2 (enExample)
CN (1) CN102387963B (enExample)
CA (1) CA2755557A1 (enExample)
GB (1) GB0906157D0 (enExample)
WO (1) WO2010116170A2 (enExample)

Families Citing this family (14)

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FR2981880B1 (fr) * 2011-10-28 2014-09-19 Daher Aerospace Procede pour etancher un reservoir de carburant
CN103434638A (zh) * 2013-09-16 2013-12-11 哈尔滨工业大学 复合材料机翼中梁与加强肋的混合连接方法
US9994298B2 (en) 2015-06-30 2018-06-12 Lockheed Martin Corporation System for embedded removable aperture
CN105627836B (zh) * 2016-02-18 2018-08-24 江西洪都航空工业集团有限责任公司 一种组合梁式翼面结构
GB2550403A (en) * 2016-05-19 2017-11-22 Airbus Operations Ltd Aerofoil body with integral curved spar-cover
US10556665B2 (en) * 2016-06-20 2020-02-11 The Boeing Company Apparatuses and methods for improved sealing
US10745147B2 (en) * 2016-11-11 2020-08-18 Bell Helicopter Textron Inc. Detachable cargo mirror
CN107244409B (zh) * 2017-05-31 2019-08-09 彩虹无人机科技有限公司 一种复合材料机翼整体油箱结构
ES2800182T3 (es) * 2017-07-13 2020-12-28 Airbus Operations Sl Disposición estructural de caja para una aeronave y procedimiento de fabricación de la misma
CN108100224B (zh) * 2018-01-17 2020-12-25 安徽中骄智能科技有限公司 一种集成电池平凸翼式无人机
CN109305328B (zh) * 2018-11-12 2024-01-16 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种翼盒及飞机
CN110525634B (zh) * 2019-09-09 2021-03-23 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种尾翼后缘舱与主盒段的连接结构
GB2587671A (en) * 2019-10-02 2021-04-07 Advanced Mobility Res And Development Ltd Systems and methods for aircraft
DE102022116949A1 (de) * 2022-07-07 2024-01-18 Airbus Operations Gmbh Tragfläche für ein Luftfahrzeug

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US7249943B2 (en) * 2003-08-01 2007-07-31 Alliant Techsystems Inc. Apparatus for forming composite stiffeners and reinforcing structures
US7264200B2 (en) * 2004-07-23 2007-09-04 The Boeing Company System and method for improved rotor tip performance
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US7686905B2 (en) * 2005-09-06 2010-03-30 The Boeing Company Copper grid repair technique for lightning strike protection
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