JPWO2021191967A5 - - Google Patents

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Publication number
JPWO2021191967A5
JPWO2021191967A5 JP2022509780A JP2022509780A JPWO2021191967A5 JP WO2021191967 A5 JPWO2021191967 A5 JP WO2021191967A5 JP 2022509780 A JP2022509780 A JP 2022509780A JP 2022509780 A JP2022509780 A JP 2022509780A JP WO2021191967 A5 JPWO2021191967 A5 JP WO2021191967A5
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JP
Japan
Prior art keywords
base material
fiber base
space
fiber
thermosetting resin
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JP2022509780A
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English (en)
Japanese (ja)
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JP7318112B2 (ja
JPWO2021191967A1 (https=
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Priority claimed from PCT/JP2020/012718 external-priority patent/WO2021191967A1/ja
Publication of JPWO2021191967A1 publication Critical patent/JPWO2021191967A1/ja
Publication of JPWO2021191967A5 publication Critical patent/JPWO2021191967A5/ja
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JP2022509780A 2020-03-23 2020-03-23 繊維強化複合材成形方法および繊維強化複合材成形装置 Active JP7318112B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2020/012718 WO2021191967A1 (ja) 2020-03-23 2020-03-23 繊維強化複合材成形方法および繊維強化複合材成形装置

Publications (3)

Publication Number Publication Date
JPWO2021191967A1 JPWO2021191967A1 (https=) 2021-09-30
JPWO2021191967A5 true JPWO2021191967A5 (https=) 2022-07-25
JP7318112B2 JP7318112B2 (ja) 2023-07-31

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JP2022509780A Active JP7318112B2 (ja) 2020-03-23 2020-03-23 繊維強化複合材成形方法および繊維強化複合材成形装置

Country Status (3)

Country Link
EP (1) EP4059688B1 (https=)
JP (1) JP7318112B2 (https=)
WO (1) WO2021191967A1 (https=)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12611823B2 (en) * 2022-12-13 2026-04-28 The Boeing Company In-tool compaction for composite structures
CN116653181B (zh) * 2023-05-26 2025-05-06 广联航空工业股份有限公司 一种复合材料制造用脱模装置及其使用方法

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3764641A (en) * 1971-01-08 1973-10-09 A Ash Method of forming irregularly shaped hollow articles using a variable stiffness mandrel
SE509503C2 (sv) * 1997-05-12 1999-02-01 Volvo Ab Arrangemang, förfarande och hålkropp vid formning av plastdetaljer
CA2347717A1 (en) * 1998-09-30 2000-04-06 Toray Industries, Inc. A fibre-reinforced resin structure having hollow cross section and manufacturing method thereof
US6889937B2 (en) * 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
US9296187B2 (en) * 2008-12-10 2016-03-29 The Boeing Company Bagging process and mandrel for fabrication of elongated composite structure
DE102009026456A1 (de) * 2009-05-25 2010-12-16 Airbus Operations Gmbh Vorrichtung und Verfahren zur Herstellung eines Verbundbauteils
JP6209095B2 (ja) * 2014-01-31 2017-10-04 三菱重工業株式会社 Frp成形治具及びfrp構造体の成形方法
GB2525243A (en) * 2014-04-17 2015-10-21 Airbus Operations Ltd A method of moulding and a core plug for use in the method
US10086534B2 (en) * 2014-10-17 2018-10-02 The Boeing Company Multifunctional mandrel end cap and method
US10926435B2 (en) * 2017-05-03 2021-02-23 The Boeing Company Foam mandrel assembly
JP6715226B2 (ja) * 2017-10-25 2020-07-01 株式会社Subaru 複合材成形治具及び複合材成形方法

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