JP2019202752A5 - - Google Patents

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Publication number
JP2019202752A5
JP2019202752A5 JP2019038502A JP2019038502A JP2019202752A5 JP 2019202752 A5 JP2019202752 A5 JP 2019202752A5 JP 2019038502 A JP2019038502 A JP 2019038502A JP 2019038502 A JP2019038502 A JP 2019038502A JP 2019202752 A5 JP2019202752 A5 JP 2019202752A5
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JP
Japan
Prior art keywords
stringer
edge
composite structure
thickness
angle
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.)
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Application number
JP2019038502A
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English (en)
Japanese (ja)
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JP2019202752A (ja
JP7455512B2 (ja
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Publication date
Priority claimed from US15/913,488 external-priority patent/US10689085B2/en
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Publication of JP2019202752A publication Critical patent/JP2019202752A/ja
Publication of JP2019202752A5 publication Critical patent/JP2019202752A5/ja
Application granted granted Critical
Publication of JP7455512B2 publication Critical patent/JP7455512B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2019038502A 2018-03-06 2019-03-04 改善した引き抜き強度を有するストリンガ補強複合パネル Active JP7455512B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/913,488 US10689085B2 (en) 2017-08-14 2018-03-06 Stringer stiffened composite panels having improved pull-off strength
US15/913,488 2018-03-06

Publications (3)

Publication Number Publication Date
JP2019202752A JP2019202752A (ja) 2019-11-28
JP2019202752A5 true JP2019202752A5 (https=) 2022-03-11
JP7455512B2 JP7455512B2 (ja) 2024-03-26

Family

ID=65685247

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2019038502A Active JP7455512B2 (ja) 2018-03-06 2019-03-04 改善した引き抜き強度を有するストリンガ補強複合パネル

Country Status (5)

Country Link
EP (1) EP3536606B8 (https=)
JP (1) JP7455512B2 (https=)
CN (1) CN110228580B (https=)
CA (1) CA3033583C (https=)
ES (1) ES2943862T3 (https=)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112173062A (zh) * 2020-09-25 2021-01-05 中国直升机设计研究所 一种复合材料一体化框梁及制造方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8993097B2 (en) * 2011-10-10 2015-03-31 The Boeing Company Tapered height curved composite stringers and corresponding panels
US9415858B2 (en) * 2012-08-28 2016-08-16 The Boeing Company Bonded and tailorable composite assembly
CN104936768B (zh) * 2012-11-20 2017-03-08 维斯塔斯风力系统有限公司 风轮机叶片及其制造方法
EP2749405B1 (en) * 2012-12-26 2016-03-23 Airbus Operations S.L. Reinforced stringer and method of manufacture thereof
US10029780B2 (en) * 2013-08-09 2018-07-24 The Boeing Company Stiffened composite panels
US9827710B2 (en) * 2014-02-04 2017-11-28 The Boeing Company Radius filler and method of manufacturing same
US20150217850A1 (en) * 2014-02-06 2015-08-06 The Boeing Company Laminated i-blade stringer
JP5950171B1 (ja) * 2015-07-27 2016-07-13 利昭 筑田 苗押さえバリ
CN106428523A (zh) * 2015-08-10 2017-02-22 空中客车美国工程有限公司 复合翼梁的纵向层片铺设
JP6949474B2 (ja) * 2016-11-24 2021-10-13 三菱重工業株式会社 複合材及び複合材の成形方法

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