JP2013513499A5 - - Google Patents

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Publication number
JP2013513499A5
JP2013513499A5 JP2012543129A JP2012543129A JP2013513499A5 JP 2013513499 A5 JP2013513499 A5 JP 2013513499A5 JP 2012543129 A JP2012543129 A JP 2012543129A JP 2012543129 A JP2012543129 A JP 2012543129A JP 2013513499 A5 JP2013513499 A5 JP 2013513499A5
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JP
Japan
Prior art keywords
patch
backing plate
vacuum
tool
rework area
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
JP2012543129A
Other languages
English (en)
Japanese (ja)
Other versions
JP2013513499A (ja
JP5721739B2 (ja
Filing date
Publication date
Priority claimed from US12/637,580 external-priority patent/US8444127B2/en
Application filed filed Critical
Publication of JP2013513499A publication Critical patent/JP2013513499A/ja
Publication of JP2013513499A5 publication Critical patent/JP2013513499A5/ja
Application granted granted Critical
Publication of JP5721739B2 publication Critical patent/JP5721739B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2012543129A 2009-12-14 2010-11-12 高温複合ツール Active JP5721739B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/637,580 US8444127B2 (en) 2009-12-14 2009-12-14 High temperature composite patch tool
US12/637,580 2009-12-14
PCT/US2010/056453 WO2011081724A1 (en) 2009-12-14 2010-11-12 High temperature composite tool

Publications (3)

Publication Number Publication Date
JP2013513499A JP2013513499A (ja) 2013-04-22
JP2013513499A5 true JP2013513499A5 (cg-RX-API-DMAC7.html) 2013-10-10
JP5721739B2 JP5721739B2 (ja) 2015-05-20

Family

ID=43836990

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012543129A Active JP5721739B2 (ja) 2009-12-14 2010-11-12 高温複合ツール

Country Status (8)

Country Link
US (2) US8444127B2 (cg-RX-API-DMAC7.html)
EP (1) EP2512786B1 (cg-RX-API-DMAC7.html)
JP (1) JP5721739B2 (cg-RX-API-DMAC7.html)
KR (2) KR101964377B1 (cg-RX-API-DMAC7.html)
CN (1) CN102725132B (cg-RX-API-DMAC7.html)
BR (1) BR112012014456B1 (cg-RX-API-DMAC7.html)
CA (1) CA2778258C (cg-RX-API-DMAC7.html)
WO (1) WO2011081724A1 (cg-RX-API-DMAC7.html)

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FR2953812B1 (fr) * 2009-12-11 2012-09-07 Airbus Operations Sas Procede de reparation d'un fuselage d'aeronef
DE102010025068B4 (de) * 2010-06-25 2016-07-28 Airbus Defence and Space GmbH Vorrichtung und Verfahren zur Herstellung von faserverstärkten Bauteilen
US8826957B2 (en) * 2012-08-31 2014-09-09 General Electric Company Methods and systems for automated ply layup for composites
US9145203B2 (en) * 2012-10-31 2015-09-29 The Boeing Company Natural laminar flow wingtip
US9446572B2 (en) * 2012-10-31 2016-09-20 The Boeing Company Composite tool having vacuum integrity
DE102012223871B4 (de) * 2012-12-20 2024-01-18 Bayerische Motoren Werke Aktiengesellschaft Verfahren für die Vorbereitung eines Halbzeugs aus Fasermaterial auf ein Nasspressverfahren sowie Vorbereitungsvorrichtung für die Vorbereitung eines Halbzeugs aus Fasermaterial auf ein Nasspressverfahren
US9308688B1 (en) * 2013-03-20 2016-04-12 The Boeing Company Installation assembly and associated method for forming a bonded joint
US9895716B2 (en) * 2013-04-17 2018-02-20 General Electric Company Repair process and a repaired component
US9227261B2 (en) * 2013-08-06 2016-01-05 Globalfoundries Inc. Vacuum carriers for substrate bonding
US9370902B2 (en) * 2013-10-03 2016-06-21 Comerstone Research Group, Inc. Fiber-reinforced epoxy composites and methods of making same without the use of oven or autoclave
JP6273804B2 (ja) * 2013-12-02 2018-02-07 東レ株式会社 繊維強化プラスチック成形体の製造方法
FR3025133B1 (fr) * 2014-08-27 2017-03-31 Airbus Operations Sas Procede de reparation d'une piece en materiau composite
US9908993B1 (en) 2014-10-06 2018-03-06 Cornerstone Research Group, Inc. Hybrid fiber layup and fiber-reinforced polymeric composites produced therefrom
GB2531600A (en) * 2014-10-24 2016-04-27 Short Brothers Plc Apparatus and methods for manufacturing and repairing fibre-reinforced composite materials
JP6463094B2 (ja) 2014-11-25 2019-01-30 三菱重工業株式会社 接合装置及び接合方法
US9960070B2 (en) * 2014-12-06 2018-05-01 Kla-Tencor Corporation Chucking warped wafer with bellows
CN104972730B (zh) * 2015-07-09 2017-01-04 福建省欧亚斯特环保建材有限公司 玻镁饰面板的生产方法
US10946594B1 (en) 2017-01-06 2021-03-16 Cornerstone Research Group, Inc. Reinforced polymer-infused fiber composite repair system and methods for repairing composite materials
US10786957B2 (en) * 2017-01-30 2020-09-29 General Electric Company System, method, and apparatus for infusing a composite structure
FR3073448B1 (fr) * 2017-11-16 2022-02-04 Safran Nacelles Procede de reparation d'un profile composite
US10843449B2 (en) * 2017-12-14 2020-11-24 The Boeing Company Method and apparatus for forming composite plies on contoured tool surfaces
EP3578293A1 (en) * 2018-06-08 2019-12-11 Nitto Belgium NV Method for attaching an element to a workpiece using an application tool and application tool for use in the method
JP7018855B2 (ja) * 2018-09-11 2022-02-14 三菱重工業株式会社 修理パッチ、修理パッチの成形方法及び複合材の修理方法
WO2020152652A1 (en) 2019-01-25 2020-07-30 National Research Council Of Canada Articulated forming caul for composite blank vacuum forming
US11701801B2 (en) * 2019-03-04 2023-07-18 The Boeing Company Caul plate with feature for separating from composite part
US11230069B2 (en) 2019-08-28 2022-01-25 Textron Innovations Inc. Tool for forming a composite member
GB201913332D0 (en) * 2019-09-16 2019-10-30 Blade Dynamics Ltd A container comprising fibre material for a fibre-reinforced composite component
US12007175B2 (en) * 2020-10-20 2024-06-11 The Boeing Company Thermal transfer blanket system
US11827821B2 (en) 2021-02-04 2023-11-28 The Boeing Company Method for curing a patch
JP7629811B2 (ja) * 2021-06-25 2025-02-14 三菱重工業株式会社 セラミックス基複合材の成形方法
US12215062B2 (en) * 2022-11-10 2025-02-04 Rolls-Royce Plc Multi-stage consolidation process for ceramic matrix composite prepreg material
US20240359413A1 (en) * 2023-04-26 2024-10-31 The Boeing Company Systems and methods for composite stringer package construction and compacted stringer packages
EP4610035A1 (en) * 2024-02-27 2025-09-03 Siemens Gamesa Renewable Energy A/S Method and clamping device for manufacturing and/or repairing a wind turbine blade

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US3377096A (en) * 1967-06-02 1968-04-09 Wood S Powr Grip Co Inc Vacuum gripping pad
US3837965A (en) * 1972-10-17 1974-09-24 Us Air Force Portable repair apparatus
US4352707A (en) * 1981-04-23 1982-10-05 Grumman Aerospace Corporation Composite repair apparatus
US4822651A (en) * 1985-08-30 1989-04-18 Newsom Cosby M Vacuum diaphragm device
GB9622780D0 (en) * 1996-11-01 1997-01-08 British Aerospace Repair of composite laminates
FR2763882B1 (fr) * 1997-05-29 1999-08-20 Aerospatiale Outillage de reparation sur site d'une structure composite presentant une zone endommagee et procede correspondant
US5971454A (en) * 1998-01-09 1999-10-26 International Business Machines Corporation Article handler
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US6761783B2 (en) * 2002-04-09 2004-07-13 The Boeing Company Process method to repair bismaleimide (BMI) composite structures
US7857925B2 (en) * 2007-06-15 2010-12-28 The Boeing Company Process development protocol and vacuum bag process for carbon-epoxy prepreg
US8109312B2 (en) * 2007-12-29 2012-02-07 Michelin Recherche Et Technique S.A. Tire patch applicator
DE102008004297A1 (de) * 2008-01-15 2009-07-16 Oerlikon Leybold Vacuum Gmbh Turbomolekularpumpe
US8545650B2 (en) * 2009-12-08 2013-10-01 The Boeing Company Method of repairing a composite structure

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