JP2022080871A5 - - Google Patents

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Publication number
JP2022080871A5
JP2022080871A5 JP2021183215A JP2021183215A JP2022080871A5 JP 2022080871 A5 JP2022080871 A5 JP 2022080871A5 JP 2021183215 A JP2021183215 A JP 2021183215A JP 2021183215 A JP2021183215 A JP 2021183215A JP 2022080871 A5 JP2022080871 A5 JP 2022080871A5
Authority
JP
Japan
Prior art keywords
composite structure
treating
tool
applying
processing tool
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.)
Pending
Application number
JP2021183215A
Other languages
English (en)
Japanese (ja)
Other versions
JP2022080871A (ja
Filing date
Publication date
Application filed filed Critical
Publication of JP2022080871A publication Critical patent/JP2022080871A/ja
Publication of JP2022080871A5 publication Critical patent/JP2022080871A5/ja
Pending legal-status Critical Current

Links

JP2021183215A 2020-11-18 2021-11-10 複合構造を処理するための装置及び方法 Pending JP2022080871A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US202063115160P 2020-11-18 2020-11-18
US63/115,160 2020-11-18

Publications (2)

Publication Number Publication Date
JP2022080871A JP2022080871A (ja) 2022-05-30
JP2022080871A5 true JP2022080871A5 (enExample) 2026-02-27

Family

ID=81587268

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2021183215A Pending JP2022080871A (ja) 2020-11-18 2021-11-10 複合構造を処理するための装置及び方法

Country Status (3)

Country Link
US (1) US12434447B2 (enExample)
JP (1) JP2022080871A (enExample)
CN (1) CN114536803A (enExample)

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2456513A (en) 1945-04-20 1948-12-14 Theodore L Johnson Molding of hollow articles
JP4346143B2 (ja) * 1999-02-24 2009-10-21 社団法人日本航空宇宙工業会 複合樹脂製品の成形方法及びその装置
US8016970B2 (en) 2007-08-02 2011-09-13 The Boeing Company Method for applying a pre-cured composite strip to a composite component to minimize inconsistencies appearing on a surface of the composite component
US8454870B2 (en) 2008-12-19 2013-06-04 The Boeing Company Manufacturing one-piece composite sections using outer mold line tooling
ITTO20100175A1 (it) * 2010-03-08 2011-09-09 Alenia Aeronautica Spa Procedimento per la fabbricazione di longheroni alari e travi di fusoliera a doppio t in materiale composito a sezione variabile
US8262841B2 (en) * 2010-11-24 2012-09-11 The Boeing Company Methods for void-free debulking of adhesive bonded joints
WO2012090468A1 (ja) * 2010-12-27 2012-07-05 川崎重工業株式会社 成形型、成形治具、および成形方法
US9314976B2 (en) * 2013-02-15 2016-04-19 The Boeing Company Systems and methods for compacting a charge of composite material
US9897440B2 (en) 2014-01-17 2018-02-20 The Boeing Company Method and system for determining and verifying ply orientation of a composite laminate
US10001365B2 (en) 2014-09-04 2018-06-19 The Boeing Company Methods and systems for forming a mandrel assembly for use with a locating system
CN105522724B (zh) * 2014-10-24 2019-06-04 波音公司 真空压实装置和对丝束进行压实的方法
DE102017107908A1 (de) 2017-04-12 2018-10-18 Herbert Funke MGI-Verfahren und entsprechendes Formwerkzeug
US11104113B2 (en) * 2017-04-19 2021-08-31 The Boeing Company Systems and methods for assembling elongate composite structures
US10766212B2 (en) 2017-12-13 2020-09-08 The Boeing Company Method and apparatus for forming radius filler kits
US11845236B2 (en) 2018-03-12 2023-12-19 The Boeing Company Composite structure splice and method
EP3628475B1 (en) * 2018-09-26 2023-07-19 The Boeing Company System and method for manufacturing composite structures
US11220353B2 (en) 2019-04-18 2022-01-11 The Boeing Company Method of fabricating a composite structure

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