JP2013534194A5 - - Google Patents

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Publication number
JP2013534194A5
JP2013534194A5 JP2013524854A JP2013524854A JP2013534194A5 JP 2013534194 A5 JP2013534194 A5 JP 2013534194A5 JP 2013524854 A JP2013524854 A JP 2013524854A JP 2013524854 A JP2013524854 A JP 2013524854A JP 2013534194 A5 JP2013534194 A5 JP 2013534194A5
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JP
Japan
Prior art keywords
openings
frame
load
airfoil
covers
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.)
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Application number
JP2013524854A
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English (en)
Japanese (ja)
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JP5823519B2 (ja
JP2013534194A (ja
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Publication date
Priority claimed from US12/857,750 external-priority patent/US8348196B2/en
Application filed filed Critical
Publication of JP2013534194A publication Critical patent/JP2013534194A/ja
Publication of JP2013534194A5 publication Critical patent/JP2013534194A5/ja
Application granted granted Critical
Publication of JP5823519B2 publication Critical patent/JP5823519B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013524854A 2010-08-17 2011-07-21 多桁ポートボックスジョイント Active JP5823519B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/857,750 2010-08-17
US12/857,750 US8348196B2 (en) 2010-08-17 2010-08-17 Multi-spar port box joint
PCT/US2011/044766 WO2012024051A1 (en) 2010-08-17 2011-07-21 Multi-spar port box joint

Publications (3)

Publication Number Publication Date
JP2013534194A JP2013534194A (ja) 2013-09-02
JP2013534194A5 true JP2013534194A5 (https=) 2014-07-17
JP5823519B2 JP5823519B2 (ja) 2015-11-25

Family

ID=44629784

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013524854A Active JP5823519B2 (ja) 2010-08-17 2011-07-21 多桁ポートボックスジョイント

Country Status (6)

Country Link
US (2) US8348196B2 (https=)
EP (1) EP2605959B1 (https=)
JP (1) JP5823519B2 (https=)
CN (1) CN103097240B (https=)
ES (1) ES2574308T3 (https=)
WO (1) WO2012024051A1 (https=)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2372828B1 (es) * 2008-12-17 2012-12-13 Airbus Operations, S.L. Costilla-herraje.
ES2372849B1 (es) * 2010-03-25 2012-12-13 Airbus Operations, S.L. Estructura de unión de cajones de torsión en una aeronave mediante un herraje triforme de materiales compuestos no metálicos.
US8348196B2 (en) 2010-08-17 2013-01-08 The Boeing Company Multi-spar port box joint
GB201020152D0 (en) * 2010-11-29 2011-01-12 Airbus Uk Ltd Aircraft panel structure and aircraft panel structure manufacturing method for alleviation of stress
US9266625B1 (en) * 2012-06-27 2016-02-23 The Boeing Company System and method for scanning a wing box skin
US9315254B2 (en) * 2013-10-11 2016-04-19 The Boeing Company Joint assembly and method of assembling same
CN105539812A (zh) * 2014-10-28 2016-05-04 中国航空工业集团公司西安飞机设计研究所 一种机翼翼梁对接接头
US9828083B2 (en) * 2014-11-14 2017-11-28 The Boeing Company Methods and components for wing-to-fuselage integration
EP3095691A1 (en) * 2015-05-22 2016-11-23 Airbus Operations, S.L. Multi-spar torsion box structure
US9994298B2 (en) 2015-06-30 2018-06-12 Lockheed Martin Corporation System for embedded removable aperture
CN106314759A (zh) * 2016-09-06 2017-01-11 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种飞机机翼的翼梁连接结构
CN110603192B (zh) * 2017-05-01 2023-06-16 庞巴迪公司 允许位置调节的飞机机翼与机身接口
US10773787B2 (en) 2017-06-14 2020-09-15 The Boeing Company Wing-to-fuselage joints and aircraft including the same
US10766598B2 (en) * 2017-06-14 2020-09-08 The Boeing Company Wing-to-fuselage joints and aircraft including the same
EP3604120B1 (en) * 2018-08-01 2022-01-26 Airbus Operations, S.L.U. Fitting for attaching the horizontal tail stabilizer of an aircraft
US11352063B2 (en) * 2018-08-30 2022-06-07 Clark Equipment Company Frame access aperture
FR3091259A1 (fr) 2018-12-26 2020-07-03 Airbus Operations Voilure d’aeronef comprenant deux ailes fixees l’une sur l’autre
US11511846B2 (en) 2020-05-27 2022-11-29 The Boeing Company Aircraft with multi spar box connection to fuselage
US11370523B2 (en) 2020-05-27 2022-06-28 The Boeing Company Aircraft with multi spar box connection to fuselage
US12404003B2 (en) 2020-08-12 2025-09-02 The Boeing Company CFRP fuselage frame with securement to vertical tail fin
US11932398B2 (en) 2020-08-24 2024-03-19 The Boeing Company Horizontal stabilizer assembly for an aircraft
US12252245B2 (en) * 2021-01-20 2025-03-18 The Boeing Company Beaded composite structures and methods for manufacturing beaded composite structures
EP4197918B1 (fr) * 2021-12-16 2024-08-21 Airbus Operations (S.A.S.) Pièce de coin flexible destinée à contribuer à une liaison entre au moins trois parois d' au moins un caisson d' aéronef
US12291330B2 (en) * 2023-08-10 2025-05-06 The Boeing Company Aircraft wing having a truss system for coupling a center wing section to an outboard wing section

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3417946A (en) 1967-12-29 1968-12-24 Lockheed Aircraft Corp T-tail construction for aircraft
US4741943A (en) 1985-12-30 1988-05-03 The Boeing Company Aerodynamic structures of composite construction
US5817269A (en) 1996-10-25 1998-10-06 The Boeing Company Composite fabrication method and tooling to improve part consolidation
US6513757B1 (en) 1999-07-19 2003-02-04 Fuji Jukogyo Kabushiki Kaisha Wing of composite material and method of fabricating the same
GB0615104D0 (en) 2006-07-28 2006-09-06 Airbus Uk Ltd Aircraft wing box and manufacture thereof
US7575194B2 (en) 2006-11-30 2009-08-18 The Boeing Company Apparatuses and methods for joining composite members and other structural members in aircraft wing boxes and other structures
ES2335837B1 (es) * 2007-06-29 2011-02-18 Airbus España, Sl. Cubierta para boca de acceso de aeronave.
US8348196B2 (en) 2010-08-17 2013-01-08 The Boeing Company Multi-spar port box joint

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