JP2016097633A5 - - Google Patents

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Publication number
JP2016097633A5
JP2016097633A5 JP2014238073A JP2014238073A JP2016097633A5 JP 2016097633 A5 JP2016097633 A5 JP 2016097633A5 JP 2014238073 A JP2014238073 A JP 2014238073A JP 2014238073 A JP2014238073 A JP 2014238073A JP 2016097633 A5 JP2016097633 A5 JP 2016097633A5
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JP
Japan
Prior art keywords
patch
pressing member
corner portion
joining
corner
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.)
Granted
Application number
JP2014238073A
Other languages
English (en)
Japanese (ja)
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JP2016097633A (ja
JP6463094B2 (ja
Filing date
Publication date
Application filed filed Critical
Priority claimed from JP2014238073A external-priority patent/JP6463094B2/ja
Priority to JP2014238073A priority Critical patent/JP6463094B2/ja
Priority to US15/507,757 priority patent/US10456961B2/en
Priority to PCT/JP2015/083112 priority patent/WO2016084861A1/ja
Priority to EP15863240.6A priority patent/EP3181339B1/en
Priority to BR112017003982A priority patent/BR112017003982A2/pt
Priority to CN201580041094.XA priority patent/CN106573422B/zh
Priority to CA2959476A priority patent/CA2959476C/en
Publication of JP2016097633A publication Critical patent/JP2016097633A/ja
Publication of JP2016097633A5 publication Critical patent/JP2016097633A5/ja
Publication of JP6463094B2 publication Critical patent/JP6463094B2/ja
Application granted granted Critical
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2014238073A 2014-11-25 2014-11-25 接合装置及び接合方法 Active JP6463094B2 (ja)

Priority Applications (7)

Application Number Priority Date Filing Date Title
JP2014238073A JP6463094B2 (ja) 2014-11-25 2014-11-25 接合装置及び接合方法
BR112017003982A BR112017003982A2 (pt) 2014-11-25 2015-11-25 aparelho de ligação, e, método de ligação para ligar um remendo contendo uma fibra de reforço em uma seção ligada de uma parte de superfície.
PCT/JP2015/083112 WO2016084861A1 (ja) 2014-11-25 2015-11-25 接合装置と接合方法
EP15863240.6A EP3181339B1 (en) 2014-11-25 2015-11-25 Bonding device and bonding method
US15/507,757 US10456961B2 (en) 2014-11-25 2015-11-25 Bonding apparatus and bonding method
CN201580041094.XA CN106573422B (zh) 2014-11-25 2015-11-25 接合装置和接合方法
CA2959476A CA2959476C (en) 2014-11-25 2015-11-25 Bonding apparatus and bonding method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2014238073A JP6463094B2 (ja) 2014-11-25 2014-11-25 接合装置及び接合方法

Publications (3)

Publication Number Publication Date
JP2016097633A JP2016097633A (ja) 2016-05-30
JP2016097633A5 true JP2016097633A5 (enExample) 2017-07-27
JP6463094B2 JP6463094B2 (ja) 2019-01-30

Family

ID=56074413

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014238073A Active JP6463094B2 (ja) 2014-11-25 2014-11-25 接合装置及び接合方法

Country Status (7)

Country Link
US (1) US10456961B2 (enExample)
EP (1) EP3181339B1 (enExample)
JP (1) JP6463094B2 (enExample)
CN (1) CN106573422B (enExample)
BR (1) BR112017003982A2 (enExample)
CA (1) CA2959476C (enExample)
WO (1) WO2016084861A1 (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10695993B2 (en) 2016-01-15 2020-06-30 GM Global Technology Operations LLC In-situ polymerization of polyamides for composite part repair
US10589477B2 (en) 2016-05-02 2020-03-17 GM Global Technology Operations LLC Cosmetic repair of a thermoplastic carbon fiber composite
US11046017B2 (en) * 2016-11-07 2021-06-29 Robert Bosch Battery Systems Llc Device and method for forming complex joints in layered sheet material
DE102017004339B4 (de) * 2017-05-05 2021-05-12 Audi Ag Verfahren zum Herstellen eines Faserverbundbauteils
US10611104B2 (en) * 2017-06-15 2020-04-07 GM Global Technology Operations LLC Heating elements for repair of molding defects for carbon fiber thermoplastic composites
JP7291536B2 (ja) * 2019-05-20 2023-06-15 日産自動車株式会社 繊維強化樹脂製のパネル及びその成形方法
JP7255025B2 (ja) * 2020-06-17 2023-04-10 三菱重工業株式会社 治具及び複合材の加工方法
KR102315158B1 (ko) * 2021-05-12 2021-10-20 오시찬 접착물 배출장치
US12011887B2 (en) 2021-12-17 2024-06-18 Rohr, Inc. Systems and methods for thermoplastic panel manufacturing
WO2024163421A1 (en) * 2023-01-31 2024-08-08 Rtx Corporation Polyimide composite repair apparatus and method via high temperature resin transfer molding

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2638673B1 (fr) * 1988-11-08 1991-03-22 Aerospatiale Outillage pour le moulage de panneaux auto-raidis en materiau composite
GB9622780D0 (en) * 1996-11-01 1997-01-08 British Aerospace Repair of composite laminates
US6761783B2 (en) * 2002-04-09 2004-07-13 The Boeing Company Process method to repair bismaleimide (BMI) composite structures
KR101220765B1 (ko) * 2004-07-16 2013-01-09 미쓰비시 가가꾸 가부시키가이샤 전자사진 감광체
US8790485B2 (en) 2005-02-25 2014-07-29 Bell Helicopter Textron Inc. Single vacuum debulk composite panel repair
US7857925B2 (en) 2007-06-15 2010-12-28 The Boeing Company Process development protocol and vacuum bag process for carbon-epoxy prepreg
EP2214893B1 (en) 2007-11-26 2013-05-29 Bell Helicopter Textron Inc. Multi-stage debulk and compaction of thick composite repair laminates
JP4929147B2 (ja) * 2007-12-19 2012-05-09 三菱重工業株式会社 樹脂製品の修理方法
DE102007062872A1 (de) * 2007-12-28 2009-07-09 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Profils aus Faserverbundwerkstoff
DE102009001075A1 (de) * 2009-02-23 2010-09-09 Airbus Deutschland Gmbh Verfahren zum zumindest teilweise Nachbearbeiten oder Ersetzen eines Versteifungselementes einer Faserverbundstruktur und zugehörige Anbindvorrichtung
US8444127B2 (en) * 2009-12-14 2013-05-21 The Boeing Company High temperature composite patch tool
IT1399682B1 (it) * 2010-03-29 2013-04-26 Alenia Aeronautica Spa Procedimento e dispositivo per la riparazione di pannelli di materiale composito
US8986479B2 (en) 2010-09-30 2015-03-24 The Boeing Company Systems and methods for on-aircraft composite repair using double vacuum debulking

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