JP2010536622A5 - - Google Patents

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Publication number
JP2010536622A5
JP2010536622A5 JP2010522027A JP2010522027A JP2010536622A5 JP 2010536622 A5 JP2010536622 A5 JP 2010536622A5 JP 2010522027 A JP2010522027 A JP 2010522027A JP 2010522027 A JP2010522027 A JP 2010522027A JP 2010536622 A5 JP2010536622 A5 JP 2010536622A5
Authority
JP
Japan
Prior art keywords
conductive
adhesive film
structural adhesive
carbon fiber
scrim
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
JP2010522027A
Other languages
English (en)
Japanese (ja)
Other versions
JP2010536622A (ja
Filing date
Publication date
Priority claimed from US11/844,174 external-priority patent/US7628879B2/en
Application filed filed Critical
Publication of JP2010536622A publication Critical patent/JP2010536622A/ja
Publication of JP2010536622A5 publication Critical patent/JP2010536622A5/ja
Pending legal-status Critical Current

Links

JP2010522027A 2007-08-23 2008-08-21 導電スクリムを組み込んだ構造用接着フィルム Pending JP2010536622A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/844,174 US7628879B2 (en) 2007-08-23 2007-08-23 Conductive scrim embedded structural adhesive films
PCT/US2008/073869 WO2009026442A1 (en) 2007-08-23 2008-08-21 Conductive scrim embedded structural adhesive films

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP2013114148A Division JP5805706B2 (ja) 2007-08-23 2013-05-30 導電スクリムを組み込んだ構造用接着フィルム

Publications (2)

Publication Number Publication Date
JP2010536622A JP2010536622A (ja) 2010-12-02
JP2010536622A5 true JP2010536622A5 (enExample) 2011-10-06

Family

ID=39791316

Family Applications (2)

Application Number Title Priority Date Filing Date
JP2010522027A Pending JP2010536622A (ja) 2007-08-23 2008-08-21 導電スクリムを組み込んだ構造用接着フィルム
JP2013114148A Active JP5805706B2 (ja) 2007-08-23 2013-05-30 導電スクリムを組み込んだ構造用接着フィルム

Family Applications After (1)

Application Number Title Priority Date Filing Date
JP2013114148A Active JP5805706B2 (ja) 2007-08-23 2013-05-30 導電スクリムを組み込んだ構造用接着フィルム

Country Status (7)

Country Link
US (1) US7628879B2 (enExample)
EP (2) EP2527415B1 (enExample)
JP (2) JP2010536622A (enExample)
CN (2) CN101910339B (enExample)
ES (2) ES2603187T3 (enExample)
PT (2) PT2183330T (enExample)
WO (1) WO2009026442A1 (enExample)

Families Citing this family (71)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7849729B2 (en) 2006-12-22 2010-12-14 The Boeing Company Leak detection in vacuum bags
US9770871B2 (en) * 2007-05-22 2017-09-26 The Boeing Company Method and apparatus for layup placement
US8568551B2 (en) 2007-05-22 2013-10-29 The Boeing Company Pre-patterned layup kit and method of manufacture
US8707766B2 (en) 2010-04-21 2014-04-29 The Boeing Company Leak detection in vacuum bags
US8936695B2 (en) 2007-07-28 2015-01-20 The Boeing Company Method for forming and applying composite layups having complex geometries
US8333864B2 (en) 2008-09-30 2012-12-18 The Boeing Company Compaction of prepreg plies on composite laminate structures
US8916010B2 (en) 2007-12-07 2014-12-23 The Boeing Company Composite manufacturing method
US8752293B2 (en) * 2007-12-07 2014-06-17 The Boeing Company Method of fabricating structures using composite modules and structures made thereby
DE102008021788A1 (de) * 2008-04-30 2009-11-12 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zum Reparieren einer Flugzeugkomponente
US8449703B2 (en) * 2009-03-09 2013-05-28 The Boeing Company Predictable bonded rework of composite structures using tailored patches
US8409384B2 (en) * 2009-03-09 2013-04-02 The Boeing Company Predictable bonded rework of composite structures
US8540909B2 (en) * 2009-03-09 2013-09-24 The Boeing Company Method of reworking an area of a composite structure containing an inconsistency
US8617694B1 (en) 2009-03-09 2013-12-31 The Boeing Company Discretely tailored multi-zone bondline for fail-safe structural repair
US8524356B1 (en) 2009-03-09 2013-09-03 The Boeing Company Bonded patch having multiple zones of fracture toughness
US9492975B2 (en) 2009-03-09 2016-11-15 The Boeing Company Structural bonded patch with tapered adhesive design
US20100233424A1 (en) * 2009-03-10 2010-09-16 The Boeing Company Composite structures employing quasi-isotropic laminates
CN102422068A (zh) * 2009-03-11 2012-04-18 迪普弗莱克斯有限公司 用于修补挠性纤维增强管子的方法和设备
US8857128B2 (en) * 2009-05-18 2014-10-14 Apple Inc. Reinforced device housing
JP5439963B2 (ja) * 2009-06-12 2014-03-12 三菱電機株式会社 ソーラーアレイパネル、ソーラーアレイパネルの補修方法
GB2474897B (en) * 2009-11-02 2015-09-16 Hexcel Composites Ltd Electromagnetic hazard protector for composite materials
US8408972B2 (en) * 2010-01-25 2013-04-02 Apple Inc. Apparatus and method for intricate cuts
US8511498B2 (en) * 2010-01-25 2013-08-20 Apple Inc. Method for manufacturing an electronic device enclosure
DE102010042970A1 (de) * 2010-05-12 2011-11-17 Airbus Operations Gmbh Strukturbauteil mit verbesserter Leitfähigkeit und mechanischer Festigkeit sowie Verfahren zu dessen Herstellung
US8372495B2 (en) 2010-05-26 2013-02-12 Apple Inc. Electronic device enclosure using sandwich construction
US9120272B2 (en) 2010-07-22 2015-09-01 Apple Inc. Smooth composite structure
JP5615165B2 (ja) * 2010-12-27 2014-10-29 三菱重工業株式会社 複合材パネル構造体及びその製造方法
FR2970238B1 (fr) * 2011-01-07 2013-01-25 Airbus Operations Sas Piece et procede de reparation d'une structure endommagee, en particulier de peau d'aeronef, ainsi qu'un kit de reparation de mise en oeuvre
US9011623B2 (en) 2011-03-03 2015-04-21 Apple Inc. Composite enclosure
WO2012154544A2 (en) * 2011-05-06 2012-11-15 Purdue Research Foundation Method and system of vacuum assisted resin transfer molding for repair of composite materials and structure
EP2753814A4 (en) 2011-09-07 2015-12-09 Afton Chemical Corp AERIAL ADDITIVE DISTRIBUTION SYSTEM
US20130143006A1 (en) * 2011-12-02 2013-06-06 The Boeing Company Reducing Porosity in Composite Structures
EP2806418A4 (en) * 2012-01-16 2015-12-16 Nec Corp MOBILE TERMINAL DEVICE
DE102012001056A1 (de) * 2012-01-20 2013-07-25 Liebherr-Aerospace Lindenberg Gmbh Fahrwerkskomponente aus einem Faserverbundwerkstoff
US9849640B2 (en) * 2012-03-28 2017-12-26 Bell Helicopter Textron Inc. Processes for repairing complex laminated composites
DE102012205633A1 (de) * 2012-04-05 2013-10-10 Airbus Operations Gmbh Verfahren und Vorrichtung zum Fügen von toleranzbehafteten Fügepartnern
US20130269998A1 (en) * 2012-04-13 2013-10-17 Apple Inc. System and method for optimizing and combining adhesive parameters
US20140117022A1 (en) * 2012-10-30 2014-05-01 The Boeing Company Composite Structures Having Bondlines with Matched Electrical Conductivity
JP6124561B2 (ja) * 2012-11-20 2017-05-10 三菱航空機株式会社 複合材の修理方法
US10407955B2 (en) 2013-03-13 2019-09-10 Apple Inc. Stiff fabric
JP6300449B2 (ja) * 2013-03-28 2018-03-28 三菱航空機株式会社 被修理部の修理方法および修理装置
CN204608330U (zh) 2013-12-20 2015-09-02 苹果公司 编织纤维带
CN103862686A (zh) * 2014-02-22 2014-06-18 李文忠 非导磁性材料的工程施工热熔性胶粘技术
JP6321429B2 (ja) * 2014-03-31 2018-05-09 学校法人大同学園 繊維強化樹脂部材の修理方法および研削方法
EP2926984B1 (de) 2014-04-03 2019-02-20 Nordex Energy GmbH Verfahren zum Reparieren eines elektrischen Heizelements eines Windenergieanlagenrotorblatts
ES2770020T3 (es) * 2014-05-01 2020-06-30 Boeing Co Elemento de parcheo unido estructural con diseño adhesivo cónico
US9545782B2 (en) * 2014-05-13 2017-01-17 The Boeing Company Method and apparatus for repairing composite materials
JP6165682B2 (ja) * 2014-06-30 2017-07-19 三菱重工業株式会社 風車の翼、および、風車の翼の修理方法
US10213964B2 (en) * 2015-05-08 2019-02-26 The Boeing Company Methods and apparatus for repairing composite materials
KR101836566B1 (ko) 2015-05-15 2018-03-08 현대자동차주식회사 도전성 접착제 및 이를 이용한 복합소재의 접합방법
DE102015110193A1 (de) * 2015-06-24 2016-12-29 Airbus Operations Gmbh Verfahren zum Schweißverbinden zweier Komponenten aus einem thermoplastischen Schichtverbundwerkstoff
GB201519877D0 (en) * 2015-11-11 2015-12-23 Short Brothers Plc Methods and patches for repairing composite laminates
GB201522539D0 (en) * 2015-12-21 2016-02-03 Hexcel Composites Ltd Improvements in or relating to electrically conducting materials
US9827688B2 (en) * 2016-01-12 2017-11-28 The Boeing Company Patch fabrication system
EP3564184B1 (en) 2016-04-08 2023-03-01 Airbus Defence and Space GmbH Structural fibre-reinforced component with lightning strike protection by using carbon nano tube mats and metallic layers
US9972896B2 (en) 2016-06-23 2018-05-15 General Electric Company Wireless aircraft engine monitoring system
JP6820753B2 (ja) * 2017-01-16 2021-01-27 三菱重工業株式会社 修理パッチの成形方法
JP6847679B2 (ja) * 2017-01-20 2021-03-24 三菱重工業株式会社 複合材の修理方法
US10710352B2 (en) * 2017-07-11 2020-07-14 The Boeing Company Structural pre-cured repair patch for repair to highly loaded primary and secondary structural components
US10864686B2 (en) 2017-09-25 2020-12-15 Apple Inc. Continuous carbon fiber winding for thin structural ribs
CN110196286A (zh) * 2018-02-26 2019-09-03 漆松林 一种对比试块
CN110196278A (zh) * 2018-02-26 2019-09-03 漆松林 一种修补质量评价方法
DK3712423T3 (da) * 2019-03-21 2023-01-30 Siemens Gamesa Renewable Energy As Fremgangsmåde til reparation af et beskadiget bjælkedæksel af en vindmøllevinge af en vindmølle
US11827821B2 (en) * 2021-02-04 2023-11-28 The Boeing Company Method for curing a patch
US11199287B1 (en) * 2021-02-23 2021-12-14 Trinity Bay Equipment Holdings, LLC Multi-layer pipe tubing repair systems and methods
US11549391B2 (en) 2021-03-22 2023-01-10 General Electric Company Component formed from hybrid material
US12090708B2 (en) 2021-12-16 2024-09-17 Textron Innovations Inc. Self heating structural adhesives for out-of-autoclave and out-of-oven curing
GB202206057D0 (en) * 2022-04-26 2022-06-08 Lm Wind Power As Wind turbine blade repair
CN115042458B (zh) * 2022-06-22 2024-06-18 沈阳飞机工业（集团）有限公司 一种可用于飞机盒段结构复合材料构件的胶接修补工艺
US12435767B2 (en) 2022-12-05 2025-10-07 Saudi Arabian Oil Company Structural health monitoring of composite structures
US12487147B2 (en) 2023-03-23 2025-12-02 Saudi Arabian Oil Company Composite wrap for pipe monitoring and repair
JP2025156842A (ja) * 2024-04-02 2025-10-15 三菱重工業株式会社 接着剤の膜厚測定方法、および接合部材の製造方法

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4352142A (en) * 1981-04-15 1982-09-28 The Boeing Company Composite aircraft structure having lightning protection
US4448838A (en) * 1981-09-04 1984-05-15 Lear Fan Corp. Graphite fiber reinforced laminate structure capable of withstanding lightning strikes
US4428867A (en) 1981-11-02 1984-01-31 Lockheed Corporation Electrically conductive structural adhesive
US4978404A (en) * 1986-07-21 1990-12-18 The Boeing Company Method for repairing a hole in a structural wall of composite material
US4839771A (en) * 1987-12-04 1989-06-13 The Boeing Company Apparatus for providing a lightning protective vehicle surface
US5338827A (en) * 1990-01-30 1994-08-16 Trw Inc. Polyimide resins useful at high temperatures
US5160771A (en) * 1990-09-27 1992-11-03 Structural Laminates Company Joining metal-polymer-metal laminate sections
GB9107766D0 (en) * 1991-04-12 1991-06-05 Short Brothers Plc A structural component
CA2099808C (en) 1992-07-06 2000-11-07 Minoru Harada Vapor-grown and graphitized carbon fibers, process for preparing same, molded members thereof, and composite members thereof
FR2728395A1 (fr) * 1994-12-16 1996-06-21 Eurocopter France Element en materiau composite avec assemblage(s) de continuite electrique a travers l'element, son procede de fabrication et son utilisation en aeronautique
GB9504372D0 (en) * 1995-03-04 1995-04-26 British Aerospace A composite laminate
US5958166A (en) * 1996-12-31 1999-09-28 Mcdonnell Douglas Corporation Method for repairing high temperature composite structures
GB9807198D0 (en) * 1998-04-04 1998-06-03 British Aerospace Adhesively bonded joints in carbon fibre composite structures
JP3666719B2 (ja) * 1998-04-20 2005-06-29 タキロン株式会社 電磁波シールド板の接合構造及び導電性接合材
US6174392B1 (en) * 1999-03-04 2001-01-16 Northrop Grumman Corporation Composite structure repair process
US7223312B2 (en) * 2000-09-21 2007-05-29 Integument Technologies, Inc. Methods and materials for reducing damage from environmental electromagnetic effects
US7432448B2 (en) * 2001-02-15 2008-10-07 Integral Technologies, Inc Low cost aircraft structures and avionics manufactured from conductive loaded resin-based materials
JP2004087824A (ja) 2002-08-27 2004-03-18 Sii Micro Parts Ltd 電気二重層キャパシタ
US6919504B2 (en) 2002-12-19 2005-07-19 3M Innovative Properties Company Flexible heat sink
US20050242471A1 (en) 2004-04-30 2005-11-03 Bhatt Sanjiv M Methods for continuously producing shaped articles
JP5305656B2 (ja) 2004-08-23 2013-10-02 モーメンティブ・パフォーマンス・マテリアルズ・インク 熱伝導性組成物およびその作製方法
JP2006219078A (ja) * 2005-02-14 2006-08-24 Honda Motor Co Ltd 航空機用複合体及び航空機の複合体構造部の製造方法
US7312608B2 (en) 2005-11-03 2007-12-25 The Boeing Company Systems and methods for inspecting electrical conductivity in composite materials
KR20080004021A (ko) 2006-07-04 2008-01-09 쓰리엠 이노베이티브 프로퍼티즈 캄파니 양면의 접착력이 서로 다른 전도성 점착 테이프 및 그제조방법

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