JP2015531326A5 - - Google Patents

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Publication number
JP2015531326A5
JP2015531326A5 JP2015536776A JP2015536776A JP2015531326A5 JP 2015531326 A5 JP2015531326 A5 JP 2015531326A5 JP 2015536776 A JP2015536776 A JP 2015536776A JP 2015536776 A JP2015536776 A JP 2015536776A JP 2015531326 A5 JP2015531326 A5 JP 2015531326A5
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JP
Japan
Prior art keywords
biasing element
tool
composite article
curing
cte
Prior art date
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Application number
JP2015536776A
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English (en)
Japanese (ja)
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JP6505602B2 (ja
JP2015531326A (ja
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Priority claimed from US13/649,013 external-priority patent/US8986484B2/en
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Publication of JP2015531326A publication Critical patent/JP2015531326A/ja
Publication of JP2015531326A5 publication Critical patent/JP2015531326A5/ja
Application granted granted Critical
Publication of JP6505602B2 publication Critical patent/JP6505602B2/ja
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JP2015536776A 2012-10-10 2013-09-12 複合部品の硬化に対する形状歪みツーリングシステム及び方法 Active JP6505602B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/649,013 US8986484B2 (en) 2012-10-10 2012-10-10 Shape-distorting tooling system and method for curing composite parts
US13/649,013 2012-10-10
PCT/US2013/059512 WO2014058561A1 (en) 2012-10-10 2013-09-12 Shape-distorting tooling system and method for curing composite parts

Publications (3)

Publication Number Publication Date
JP2015531326A JP2015531326A (ja) 2015-11-02
JP2015531326A5 true JP2015531326A5 (enExample) 2016-10-20
JP6505602B2 JP6505602B2 (ja) 2019-04-24

Family

ID=49261782

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015536776A Active JP6505602B2 (ja) 2012-10-10 2013-09-12 複合部品の硬化に対する形状歪みツーリングシステム及び方法

Country Status (5)

Country Link
US (2) US8986484B2 (enExample)
EP (1) EP2906402B1 (enExample)
JP (1) JP6505602B2 (enExample)
CN (1) CN104718058B (enExample)
WO (1) WO2014058561A1 (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160375668A1 (en) * 2014-07-09 2016-12-29 Sikorsky Aircraft Corporation Method of forming a composite structure
US9981367B2 (en) * 2015-07-07 2018-05-29 The Boeing Company Exterior indexing process and tooling
US9987659B2 (en) 2015-10-19 2018-06-05 United Technologies Corporation Nanotube enhancement of interlaminar performance for a composite component
US10196140B2 (en) * 2016-04-12 2019-02-05 Sikorsky Aircraft Corporation Methods for separating rotor blade cuffs from rotor blade bodies
DK179701B1 (en) * 2017-09-06 2019-04-02 Blade Repair Solutions Ivs A method for reinforcing a wind turbine blade
US10654208B2 (en) * 2017-09-20 2020-05-19 Bell Helicopter Textron Inc. Assembly fixture with anisotropic thermal properties
US10654199B2 (en) * 2017-12-14 2020-05-19 The Boeing Company Induction heating cells with cauls over mandrels methods of using thereof

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3361608A (en) * 1963-05-20 1968-01-02 Owens Corning Fiberglass Corp Method and apparatus for producing metal-foil clad synthetic resin laminates
US4223429A (en) * 1978-09-01 1980-09-23 Robinson Helicopter Company Process for bonding main rotor blades from parts having different coefficients of thermal expansion
US4314866A (en) * 1980-12-09 1982-02-09 Lockheed Corporation Method for elevated-temperature bonding of material with different coefficients of thermal expansion
FR2587271B1 (fr) 1985-09-13 1987-12-18 Peugeot Procede de moulage de pieces en materiau plastique comportant un insert metallique et produits obtenus par ce procede
GB8621236D0 (en) * 1986-09-03 1987-01-14 Advanced Composite Components Moulding fibre reinforced laminates
JPH01272440A (ja) * 1988-04-26 1989-10-31 Fuji Heavy Ind Ltd 複合材成形品用成形型
DE19813592A1 (de) * 1998-03-27 1999-09-30 Audi Ag Flächiger Verbundkörper, insbesondere Kraftfahrzeug-Karosserieelement
GB0024121D0 (en) * 2000-10-03 2000-11-15 Bae Systems Plc Predicting behaviour of a moulded composite component
EP1543941B1 (en) 2003-12-16 2006-06-28 Airbus Espana, S.L. Process and tooling for reducing thermally induced residual stresses and shape distortions in monolithic composite structures
ES2276569B1 (es) * 2004-12-30 2008-06-16 Airbus España S.L. Util hibrido para el curado de piezas de material compuesto.
FR2898539B1 (fr) * 2006-03-20 2008-05-23 Eads Ccr Groupement D Interet Procede de realisation de panneaux raidis en materiau composite et panneaux ainsi realises
US7854874B2 (en) * 2006-11-20 2010-12-21 The Boeing Company Apparatus and methods for forming hat stiffened composite parts using thermally expansive tooling cauls
US7968021B2 (en) 2007-07-31 2011-06-28 The Boeing Company Coefficient of thermal expansion control structure
WO2009078871A1 (en) 2007-12-18 2009-06-25 Bell Helicopter Textron Inc. Rotor blade and method of making same
US7909597B2 (en) 2008-01-09 2011-03-22 The Boeing Company Cure growth control apparatus
WO2011009462A1 (en) * 2009-07-23 2011-01-27 Vestas Wind Systems A/S Method for making a mould for a wind turbine rotor blade
US20110194941A1 (en) * 2010-02-05 2011-08-11 United Technologies Corporation Co-cured sheath for composite blade
GB201016869D0 (en) 2010-10-07 2010-11-17 Rolls Royce Plc Methods and apparatus for forming a composite component
GB201102406D0 (en) 2011-02-11 2011-03-30 Rolls Royce Plc Apparatus for forming a composite component
JP5786352B2 (ja) * 2011-02-15 2015-09-30 三菱レイヨン株式会社 繊維強化樹脂板材の製造方法

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