JP2016153216A5 - - Google Patents

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Publication number
JP2016153216A5
JP2016153216A5 JP2015201875A JP2015201875A JP2016153216A5 JP 2016153216 A5 JP2016153216 A5 JP 2016153216A5 JP 2015201875 A JP2015201875 A JP 2015201875A JP 2015201875 A JP2015201875 A JP 2015201875A JP 2016153216 A5 JP2016153216 A5 JP 2016153216A5
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JP
Japan
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fiber
cte
region
ply
angle
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JP2015201875A
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English (en)
Japanese (ja)
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JP2016153216A (ja
JP6709032B2 (ja
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Priority claimed from US14/520,195 external-priority patent/US9738054B2/en
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Publication of JP2016153216A5 publication Critical patent/JP2016153216A5/ja
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JP2015201875A 2014-10-21 2015-10-13 ファイバーステアリングを使用した複合材積層板の適合された熱膨張率 Active JP6709032B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US14/520,195 2014-10-21
US14/520,195 US9738054B2 (en) 2014-10-21 2014-10-21 Tailored coefficient of thermal expansion of composite laminates using fiber steering

Publications (3)

Publication Number Publication Date
JP2016153216A JP2016153216A (ja) 2016-08-25
JP2016153216A5 true JP2016153216A5 (enExample) 2018-11-29
JP6709032B2 JP6709032B2 (ja) 2020-06-10

Family

ID=54557218

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015201875A Active JP6709032B2 (ja) 2014-10-21 2015-10-13 ファイバーステアリングを使用した複合材積層板の適合された熱膨張率

Country Status (4)

Country Link
US (2) US9738054B2 (enExample)
EP (1) EP3012099A1 (enExample)
JP (1) JP6709032B2 (enExample)
CN (1) CN105522326B (enExample)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9738054B2 (en) 2014-10-21 2017-08-22 The Boeing Company Tailored coefficient of thermal expansion of composite laminates using fiber steering
US10549491B2 (en) 2017-09-06 2020-02-04 The Boeing Company System and method for edge length differential measurement for fiber steering in automated fiber placement
US11207801B2 (en) * 2019-09-06 2021-12-28 Eagle Technology Systems and methods for making and/or using composite tube structures formed of hybrid laminates
US11400687B2 (en) 2020-03-19 2022-08-02 Eagle Technology, Llc CTE-matched hybrid tube laminate doubler

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH1016072A (ja) * 1996-06-26 1998-01-20 Japan Steel Works Ltd:The 複合材料の製造方法
US6180241B1 (en) * 1998-08-18 2001-01-30 Lucent Technologies Inc. Arrangement for reducing bending stress in an electronics package
US6893732B1 (en) * 1999-07-23 2005-05-17 American Superconductor Corporation Multi-layer articles and methods of making same
AUPS112202A0 (en) * 2002-03-14 2002-04-18 Commonwealth Scientific And Industrial Research Organisation Semiconductor manufacture
AU2003229708A1 (en) * 2003-03-06 2004-09-28 Vestas Wind Systems A/S Wind turbine blade, spar for wind turbine blade and method of preparing these
CN1914024B (zh) * 2004-01-26 2011-06-29 沙伯基础创新塑料知识产权有限公司 结构增强的树脂制品及其制备方法
US7243055B2 (en) * 2004-01-28 2007-07-10 The Boeing Company Composite stacking sequence optimization for multi-zoned composites
US20080160274A1 (en) 2006-12-31 2008-07-03 Chi Hung Dang Coefficient of thermal expansion adaptor
US8756037B2 (en) 2011-06-20 2014-06-17 The Boeing Company Curved fiber paths for composite laminates
US9738054B2 (en) 2014-10-21 2017-08-22 The Boeing Company Tailored coefficient of thermal expansion of composite laminates using fiber steering

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