JP2014534924A5 - - Google Patents

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Publication number
JP2014534924A5
JP2014534924A5 JP2014534567A JP2014534567A JP2014534924A5 JP 2014534924 A5 JP2014534924 A5 JP 2014534924A5 JP 2014534567 A JP2014534567 A JP 2014534567A JP 2014534567 A JP2014534567 A JP 2014534567A JP 2014534924 A5 JP2014534924 A5 JP 2014534924A5
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JP
Japan
Prior art keywords
continuous
curved
web
straight
web height
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JP2014534567A
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English (en)
Japanese (ja)
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JP6039676B2 (ja
JP2014534924A (ja
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Priority claimed from US13/269,839 external-priority patent/US8993097B2/en
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Publication of JP2014534924A publication Critical patent/JP2014534924A/ja
Publication of JP2014534924A5 publication Critical patent/JP2014534924A5/ja
Application granted granted Critical
Publication of JP6039676B2 publication Critical patent/JP6039676B2/ja
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JP2014534567A 2011-10-10 2012-08-29 高さが先細になる湾曲複合ストリンガーおよび対応するパネル Active JP6039676B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/269,839 US8993097B2 (en) 2011-10-10 2011-10-10 Tapered height curved composite stringers and corresponding panels
US13/269,839 2011-10-10
PCT/US2012/052894 WO2013055459A1 (en) 2011-10-10 2012-08-29 Tapered height curved composite stringers and corresponding panels

Publications (3)

Publication Number Publication Date
JP2014534924A JP2014534924A (ja) 2014-12-25
JP2014534924A5 true JP2014534924A5 (https=) 2015-09-03
JP6039676B2 JP6039676B2 (ja) 2016-12-07

Family

ID=46826927

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014534567A Active JP6039676B2 (ja) 2011-10-10 2012-08-29 高さが先細になる湾曲複合ストリンガーおよび対応するパネル

Country Status (7)

Country Link
US (1) US8993097B2 (https=)
EP (2) EP2766258B1 (https=)
JP (1) JP6039676B2 (https=)
CN (1) CN103874629B (https=)
ES (2) ES2654855T3 (https=)
RU (1) RU2600416C2 (https=)
WO (1) WO2013055459A1 (https=)

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US8684311B2 (en) * 2012-03-07 2014-04-01 The Boeing Company Bonded splice joint
FR3006297B1 (fr) * 2013-05-29 2016-07-15 Airbus Operations Sas Procede d'assemblage de deux panneaux comportant des raidisseurs a l'aide d'eclisses et aeronef comprenant une zone de jonction amelioree entre une poutre ventrale et une barque avant
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
US10086922B2 (en) 2013-11-15 2018-10-02 The Boeing Company Low stress stiffener runout in Pi bonded structure
WO2015094059A1 (en) * 2013-12-20 2015-06-25 Saab Ab Stiffening element and reinforced structure
GB2528080A (en) * 2014-07-08 2016-01-13 Airbus Operations Ltd Structure
US9586667B2 (en) * 2014-12-02 2017-03-07 The Boeing Company Splice assembly for joining structural components
US10286623B2 (en) 2015-06-15 2019-05-14 Lockheed Martin Corporation Composite materials with tapered reinforcements
US10040536B2 (en) * 2015-09-17 2018-08-07 The Boeing Company Wing structure, stringer structure, and related apparatus and methods of assembly
US9897130B2 (en) 2016-04-15 2018-02-20 The Boeing Company Telescoping cap assembly for encapsulating a fastener disposed within a confined space
US10087970B2 (en) 2016-04-29 2018-10-02 The Boeing Company Sealant Containment Assembly
US10556665B2 (en) 2016-06-20 2020-02-11 The Boeing Company Apparatuses and methods for improved sealing
GB2566920A (en) * 2017-07-12 2019-04-03 Safran Nacelles Ltd Fitting for a stiffened panel
US11014644B2 (en) 2017-10-25 2021-05-25 The Boeing Company Stiffened-cavity for modular wrap ply assembly for hat stringer
CA3033583C (en) * 2018-03-06 2023-08-15 The Boeing Company Stringer stiffened composite panels having improved pull-off strength
US11845236B2 (en) 2018-03-12 2023-12-19 The Boeing Company Composite structure splice and method
US11312468B2 (en) * 2018-08-08 2022-04-26 The Boeing Company Elongate structures, structural assemblies with elongate structures, and methods for supporting a structural load
US11180238B2 (en) * 2018-11-19 2021-11-23 The Boeing Company Shear ties for aircraft wing
US11325688B2 (en) * 2019-05-09 2022-05-10 The Boeing Company Composite stringer and methods for forming a composite stringer
US11673692B2 (en) * 2019-12-13 2023-06-13 The Boeing Company Forming tool and methods for forming a curvature into a composite stiffener
US11858623B2 (en) 2021-09-13 2024-01-02 The Boeing Company Aircraft fuel tank joints and methods of assembling the same
KR20240148479A (ko) * 2023-04-04 2024-10-11 현대자동차주식회사 동체의 날개 하중 지지구조

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GB8621725D0 (en) 1986-09-09 1986-10-15 British Aerospace Forming elongate structural components
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7134629B2 (en) 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7431196B2 (en) 2005-03-21 2008-10-07 The Boeing Company Method and apparatus for forming complex contour structural assemblies
JP5116282B2 (ja) 2006-10-31 2013-01-09 株式会社ジャムコ 構造部材の連続製造方法
DE102007029500B4 (de) * 2007-06-25 2013-02-14 Airbus Operations Gmbh Verfahren zum Koppeln von Versteifungsprofilelementen sowie Strukturbauteil
GB0712552D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Elongate composite structural members and improvements therein
GB0712549D0 (en) 2007-06-29 2007-08-08 Airbus Uk Ltd Improvements in elongate composite structural members
GB0712553D0 (en) * 2007-06-29 2007-08-08 Airbus Uk Ltd Composite panel stiffener
DE102007033868B4 (de) * 2007-07-20 2013-01-31 Airbus Operations Gmbh Profil mit wenigstens einem Hohlprofilquerschnitt
US7968169B2 (en) * 2007-08-07 2011-06-28 The Boeing Company Compound contoured composite beams and fabrication methods
FR2922517B1 (fr) * 2007-10-18 2010-04-23 Airbus France Avion comportant des jonctions d'arrets de raidisseurs et procede de fabrication d'un tel avion
US8152948B2 (en) 2008-01-09 2012-04-10 The Boeing Company Contoured composite parts
DE102008057247B3 (de) 2008-11-13 2010-01-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Paneel in einer Semimonocoque-Bauweise und Herstellungsverfahren dafür
DE102009056994B4 (de) 2009-12-04 2020-03-19 Airbus Defence and Space GmbH Stoßverbindung zwischen Rumpfsektionen und Verfahren

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