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
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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 (https=) 2016-10-20
JP6505602B2 JP6505602B2 (ja) 2019-04-24

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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 (https=)
EP (1) EP2906402B1 (https=)
JP (1) JP6505602B2 (https=)
CN (1) CN104718058B (https=)
WO (1) WO2014058561A1 (https=)

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

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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
ES2271513T3 (es) 2003-12-16 2007-04-16 Airbus España, S.L. Proceso y utillaje para reducir las tensiones residuales y las distorsiones de la forma inducidas termicamente en estructuras de composite monoliticas.
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
CN101903240B (zh) 2007-12-18 2013-08-07 贝尔直升机泰克斯特龙公司 旋翼叶片及其制造方法
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
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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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