JP2015016660A5 - - Google Patents

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Publication number
JP2015016660A5
JP2015016660A5 JP2013146641A JP2013146641A JP2015016660A5 JP 2015016660 A5 JP2015016660 A5 JP 2015016660A5 JP 2013146641 A JP2013146641 A JP 2013146641A JP 2013146641 A JP2013146641 A JP 2013146641A JP 2015016660 A5 JP2015016660 A5 JP 2015016660A5
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JP
Japan
Prior art keywords
manufacturing
reinforcing structure
skin
stringer
protective material
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
JP2013146641A
Other languages
English (en)
Japanese (ja)
Other versions
JP6204092B2 (ja
JP2015016660A (ja
Filing date
Publication date
Application filed filed Critical
Priority claimed from JP2013146641A external-priority patent/JP6204092B2/ja
Priority to JP2013146641A priority Critical patent/JP6204092B2/ja
Priority to PCT/JP2014/067008 priority patent/WO2015005125A1/ja
Priority to US14/901,822 priority patent/US9849965B2/en
Priority to EP14823339.8A priority patent/EP3020540A4/en
Priority to BR112015032624A priority patent/BR112015032624A2/pt
Priority to CA2917796A priority patent/CA2917796C/en
Publication of JP2015016660A publication Critical patent/JP2015016660A/ja
Publication of JP2015016660A5 publication Critical patent/JP2015016660A5/ja
Publication of JP6204092B2 publication Critical patent/JP6204092B2/ja
Application granted granted Critical
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013146641A 2013-07-12 2013-07-12 補強構造体の製造方法 Active JP6204092B2 (ja)

Priority Applications (6)

Application Number Priority Date Filing Date Title
JP2013146641A JP6204092B2 (ja) 2013-07-12 2013-07-12 補強構造体の製造方法
BR112015032624A BR112015032624A2 (pt) 2013-07-12 2014-06-26 método de fabricação de uma estrutura de reforço
US14/901,822 US9849965B2 (en) 2013-07-12 2014-06-26 Manufacturing method of reinforced structure
EP14823339.8A EP3020540A4 (en) 2013-07-12 2014-06-26 Method for producing reinforcing structure
PCT/JP2014/067008 WO2015005125A1 (ja) 2013-07-12 2014-06-26 補強構造体の製造方法
CA2917796A CA2917796C (en) 2013-07-12 2014-06-26 Manufacturing method of reinforced structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2013146641A JP6204092B2 (ja) 2013-07-12 2013-07-12 補強構造体の製造方法

Publications (3)

Publication Number Publication Date
JP2015016660A JP2015016660A (ja) 2015-01-29
JP2015016660A5 true JP2015016660A5 (enExample) 2016-08-25
JP6204092B2 JP6204092B2 (ja) 2017-09-27

Family

ID=52279811

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013146641A Active JP6204092B2 (ja) 2013-07-12 2013-07-12 補強構造体の製造方法

Country Status (6)

Country Link
US (1) US9849965B2 (enExample)
EP (1) EP3020540A4 (enExample)
JP (1) JP6204092B2 (enExample)
BR (1) BR112015032624A2 (enExample)
CA (1) CA2917796C (enExample)
WO (1) WO2015005125A1 (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6204093B2 (ja) 2013-07-12 2017-09-27 三菱重工業株式会社 補強構造体の製造方法
JP6204092B2 (ja) 2013-07-12 2017-09-27 三菱重工業株式会社 補強構造体の製造方法
US10472473B2 (en) * 2015-05-26 2019-11-12 The Boeing Company Enhancing z-conductivity in carbon fiber reinforced plastic composite layups
DE102017126052A1 (de) 2017-11-08 2019-05-09 Airbus Operations Gmbh Versteifungsanordnung für eine Öffnung in einer Flugzeugstruktur
JP7511354B2 (ja) * 2020-02-12 2024-07-05 三菱重工業株式会社 複合材料構造体
IT202000018139A1 (it) * 2020-07-27 2022-01-27 Leonardo Spa Procedimento per la fabbricazione di un componente strutturale in materiale composito irrigidito con almeno un corrente
GB2615755A (en) * 2022-02-15 2023-08-23 Airbus Operations Ltd Fuel tank stringer with flow passage
CN116834321B (zh) * 2023-06-06 2025-07-11 四川腾凤科技有限公司 一种复合材料板筋胶接加强的工艺方法

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4786426B2 (ja) * 2005-10-06 2011-10-05 三菱重工業株式会社 ファスナ
CA2660326A1 (en) 2006-08-17 2008-02-21 Airbus Deutschland Gmbh Production method for a workpiece composed of a fibre-composite material, and a fibre-composite component in the form of a profile with a profile cross section which varies over its length
US8900496B2 (en) * 2006-10-13 2014-12-02 The Boeing Company Edge seals for composite structure fuel tanks
FR2909919B1 (fr) * 2006-12-13 2012-12-07 Eads Ccr Procede de fabrication d'une piece complexe en materiau composite a fibres longues et a matrice thermodurcissable
DE102007015517A1 (de) 2007-03-30 2008-10-02 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Strukturbauteils
US8834668B2 (en) * 2008-11-19 2014-09-16 The Boeing Company Staged cocuring of composite structures
EP2251250A1 (en) * 2009-05-05 2010-11-17 Sika Technology AG Bonding with adhesive beads or plots
GB0912015D0 (en) * 2009-07-10 2009-08-19 Airbus Operations Ltd Stringer
DE102010042970A1 (de) * 2010-05-12 2011-11-17 Airbus Operations Gmbh Strukturbauteil mit verbesserter Leitfähigkeit und mechanischer Festigkeit sowie Verfahren zu dessen Herstellung
JP5808111B2 (ja) * 2011-02-04 2015-11-10 三菱重工業株式会社 航空機用複合材構造体、これを備えた航空機主翼および航空機胴体
JP5751871B2 (ja) * 2011-03-10 2015-07-22 三菱重工業株式会社 燃料タンク
ES2415773B1 (es) 2011-12-29 2014-09-02 Airbus Operations S.L. Método de fabricación de piezas de material compuesto con cambios de espesor
JP6204093B2 (ja) 2013-07-12 2017-09-27 三菱重工業株式会社 補強構造体の製造方法
JP6204092B2 (ja) 2013-07-12 2017-09-27 三菱重工業株式会社 補強構造体の製造方法
US9403350B2 (en) * 2013-12-16 2016-08-02 The Nordam Group, Inc. Flash control metal bonding

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