JP7455512B2 - 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 - Google Patents

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 Download PDF

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Publication number
JP7455512B2
JP7455512B2 JP2019038502A JP2019038502A JP7455512B2 JP 7455512 B2 JP7455512 B2 JP 7455512B2 JP 2019038502 A JP2019038502 A JP 2019038502A JP 2019038502 A JP2019038502 A JP 2019038502A JP 7455512 B2 JP7455512 B2 JP 7455512B2
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JP
Japan
Prior art keywords
stringer
ply
edge
exemplary
chamfer
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Active
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JP2019038502A
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English (en)
Japanese (ja)
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JP2019202752A5 (https=
JP2019202752A (ja
Inventor
フォルザン ビフザードプール，
ジアンティエン チェン，
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
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Boeing Co
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Publication date
Priority claimed from US15/913,488 external-priority patent/US10689085B2/en
Application filed by Boeing Co filed Critical Boeing Co
Publication of JP2019202752A publication Critical patent/JP2019202752A/ja
Publication of JP2019202752A5 publication Critical patent/JP2019202752A5/ja
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Publication of JP7455512B2 publication Critical patent/JP7455512B2/ja
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/302—Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0003—Producing profiled members, e.g. beams
    • B29D99/0005—Producing noodles, i.e. composite gap fillers, characterised by their construction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/182—Stringers, longerons
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
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 JP2019202752A5 (https=) 2022-03-11
JP7455512B2 true 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

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016534295A (ja) 2013-08-09 2016-11-04 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 補強複合材パネル

Family Cites Families (9)

* 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
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

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2016534295A (ja) 2013-08-09 2016-11-04 ザ・ボーイング・カンパニーＴｈｅ Ｂｏｅｉｎｇ Ｃｏｍｐａｎｙ 補強複合材パネル

Also Published As

Publication number Publication date
CA3033583C (en) 2023-08-15
JP2019202752A (ja) 2019-11-28
CA3033583A1 (en) 2019-09-06
ES2943862T3 (es) 2023-06-16
EP3536606B8 (en) 2023-03-29
EP3536606A1 (en) 2019-09-11
CN110228580A (zh) 2019-09-13
EP3536606B1 (en) 2023-02-22
CN110228580B (zh) 2024-07-19

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