JP2015533111A5 - - Google Patents

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Publication number
JP2015533111A5
JP2015533111A5 JP2015536842A JP2015536842A JP2015533111A5 JP 2015533111 A5 JP2015533111 A5 JP 2015533111A5 JP 2015536842 A JP2015536842 A JP 2015536842A JP 2015536842 A JP2015536842 A JP 2015536842A JP 2015533111 A5 JP2015533111 A5 JP 2015533111A5
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JP
Japan
Prior art keywords
wing box
aircraft
attachment member
attaching
aircraft fuselage
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
JP2015536842A
Other languages
English (en)
Japanese (ja)
Other versions
JP6159409B2 (ja
JP2015533111A (ja
Filing date
Publication date
Priority claimed from US13/652,975 external-priority patent/US8857765B2/en
Application filed filed Critical
Publication of JP2015533111A publication Critical patent/JP2015533111A/ja
Publication of JP2015533111A5 publication Critical patent/JP2015533111A5/ja
Application granted granted Critical
Publication of JP6159409B2 publication Critical patent/JP6159409B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2015536842A 2012-10-16 2013-10-08 航空機胴体フレームをウィングボックスに取り付ける方法及び装置 Active JP6159409B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/652,975 2012-10-16
US13/652,975 US8857765B2 (en) 2012-10-16 2012-10-16 Method and apparatus for attaching an aircraft fuselage frame to a wing box
PCT/US2013/063913 WO2014062423A1 (en) 2012-10-16 2013-10-08 Method and apparatus for attaching an aircraft fuselage frame to a wing box

Publications (3)

Publication Number Publication Date
JP2015533111A JP2015533111A (ja) 2015-11-19
JP2015533111A5 true JP2015533111A5 (enExample) 2016-07-07
JP6159409B2 JP6159409B2 (ja) 2017-07-05

Family

ID=49385426

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015536842A Active JP6159409B2 (ja) 2012-10-16 2013-10-08 航空機胴体フレームをウィングボックスに取り付ける方法及び装置

Country Status (5)

Country Link
US (1) US8857765B2 (enExample)
EP (1) EP2909085B1 (enExample)
JP (1) JP6159409B2 (enExample)
CN (1) CN104603007B (enExample)
WO (1) WO2014062423A1 (enExample)

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FR2998868B1 (fr) * 2012-11-30 2016-02-05 Airbus Operations Sas Dispositif de fixation intermediaire entre un fuselage d'aeronef et un train d'atterrissage d'aeronef
US9828083B2 (en) 2014-11-14 2017-11-28 The Boeing Company Methods and components for wing-to-fuselage integration
US10106240B2 (en) 2015-07-13 2018-10-23 The Boeing Company Pinned fuselage-to-wing connection
US10275565B2 (en) 2015-11-06 2019-04-30 The Boeing Company Advanced automated process for the wing-to-body join of an aircraft with predictive surface scanning
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US11136107B2 (en) * 2018-10-05 2021-10-05 The Boeing Company Method and apparatus for attaching a fuselage frame to a wing box
US11174042B2 (en) 2018-10-09 2021-11-16 The Boeing Company Wing join system and method for a wing assembly
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