JP2018070142A5 - - Google Patents

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Publication number
JP2018070142A5
JP2018070142A5 JP2017159997A JP2017159997A JP2018070142A5 JP 2018070142 A5 JP2018070142 A5 JP 2018070142A5 JP 2017159997 A JP2017159997 A JP 2017159997A JP 2017159997 A JP2017159997 A JP 2017159997A JP 2018070142 A5 JP2018070142 A5 JP 2018070142A5
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JP
Japan
Prior art keywords
panel
reinforcing material
axial load
aircraft
body 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
JP2017159997A
Other languages
English (en)
Japanese (ja)
Other versions
JP6930876B2 (ja
JP2018070142A (ja
Filing date
Publication date
Priority claimed from US15/264,209 external-priority patent/US10696373B2/en
Application filed filed Critical
Publication of JP2018070142A publication Critical patent/JP2018070142A/ja
Publication of JP2018070142A5 publication Critical patent/JP2018070142A5/ja
Application granted granted Critical
Publication of JP6930876B2 publication Critical patent/JP6930876B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2017159997A 2016-09-13 2017-08-23 航空機翼及び当該航空機翼を含む航空機 Active JP6930876B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/264,209 2016-09-13
US15/264,209 US10696373B2 (en) 2016-09-13 2016-09-13 Aircraft wings and aircraft including such aircraft wings

Publications (3)

Publication Number Publication Date
JP2018070142A JP2018070142A (ja) 2018-05-10
JP2018070142A5 true JP2018070142A5 (enExample) 2020-10-08
JP6930876B2 JP6930876B2 (ja) 2021-09-01

Family

ID=59846523

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2017159997A Active JP6930876B2 (ja) 2016-09-13 2017-08-23 航空機翼及び当該航空機翼を含む航空機

Country Status (6)

Country Link
US (1) US10696373B2 (enExample)
EP (1) EP3293107B1 (enExample)
JP (1) JP6930876B2 (enExample)
CN (1) CN107813921B (enExample)
ES (1) ES2833900T3 (enExample)
RU (1) RU2745876C2 (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10745104B2 (en) * 2018-03-02 2020-08-18 The Boeing Company Stringer transition through a common base charge
US11038334B2 (en) * 2019-01-14 2021-06-15 The Boeing Company Aircraft wing composite ribs having electrical grounding paths
US11260954B2 (en) 2019-10-09 2022-03-01 The Boeing Company Apparatus for attaching aircraft wing structural components
US11319051B2 (en) * 2020-01-03 2022-05-03 The Boeing Company Stiffened composite ribs
US11584502B2 (en) 2020-07-29 2023-02-21 The Boeing Company Composite fabric hat stringers having interleafed tape plies
US12319398B2 (en) * 2020-11-18 2025-06-03 The Boeing Company Fabrication of multi-segment spars
CN114261506B (zh) * 2021-12-31 2024-06-07 中国航空工业集团公司西安飞机设计研究所 一种具有整体油箱的复合材料机翼
KR20240148146A (ko) * 2023-04-03 2024-10-11 현대자동차주식회사 날개 프레임 및 이를 포함하는 비행기

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2367750A (en) * 1941-01-17 1945-01-23 Central Aircraft Corp Aircraft construction
GB2312483B (en) * 1996-04-24 2000-02-23 British Aerospace Joint assemblies
US8720825B2 (en) 2005-03-31 2014-05-13 The Boeing Company Composite stiffeners for aerospace vehicles
US7837148B2 (en) * 2006-06-13 2010-11-23 The Boeing Company Composite wing-body joint
GB0613949D0 (en) * 2006-07-13 2006-08-23 Airbus Uk Ltd A wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof
US7546979B1 (en) * 2006-09-15 2009-06-16 The Boeing Company Trapezoidal panel pin joint allowing free deflection between fuselage and wing
US7635106B2 (en) * 2006-11-30 2009-12-22 The Boeing Company Composite shear tie
US7721995B2 (en) * 2006-12-13 2010-05-25 The Boeing Company Rib support for wing panels
US7686251B2 (en) * 2006-12-13 2010-03-30 The Boeing Company Rib support for wing panels
ES2346834B1 (es) * 2007-04-30 2011-08-17 Airbus Operations, S.L. Estructura de costilla para cajones de torsion de un ala o de un estabilizador de una aeronave.
GB0813584D0 (en) * 2008-07-25 2008-09-03 Airbus Uk Ltd Method of stiffening a rib
WO2011071939A2 (en) 2009-12-07 2011-06-16 Global Aerosystems, Llc Wing spar splice joint
GB201009922D0 (en) * 2010-06-14 2010-07-21 Airbus Uk Ltd Aircraft wing box joint
CA2820004C (en) * 2010-12-28 2016-02-16 Bell Helicopter Textron Inc. Multi-directional load joint system
US8684311B2 (en) * 2012-03-07 2014-04-01 The Boeing Company Bonded splice joint
US9272769B2 (en) 2012-11-13 2016-03-01 The Boeing Company Joint for composite wings
US9527575B2 (en) 2012-11-26 2016-12-27 The Boeing Company Multi-box wing spar and skin
US10479475B2 (en) * 2013-08-09 2019-11-19 The Boeing Company Composite stringer beam joint structure of an aircraft
US9475570B2 (en) * 2013-08-23 2016-10-25 The Boeing Company Upper joints between outboard wing boxes and wing center sections of aircraft wing assemblies
JP6090931B2 (ja) * 2013-10-02 2017-03-08 三菱重工業株式会社 継手及び航空機構造
EP3040268A1 (en) * 2014-12-30 2016-07-06 Airbus Operations, S.L. Stringer stiffened aircraft composite structures
US10040537B2 (en) * 2015-01-15 2018-08-07 The Boeing Company Laminate composite wing structures

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