JP2008531337A5 - - Google Patents

Download PDF

Info

Publication number
JP2008531337A5
JP2008531337A5 JP2007557158A JP2007557158A JP2008531337A5 JP 2008531337 A5 JP2008531337 A5 JP 2008531337A5 JP 2007557158 A JP2007557158 A JP 2007557158A JP 2007557158 A JP2007557158 A JP 2007557158A JP 2008531337 A5 JP2008531337 A5 JP 2008531337A5
Authority
JP
Japan
Prior art keywords
laminate
impregnated
vacuum
temperature
heating
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.)
Abandoned
Application number
JP2007557158A
Other languages
English (en)
Japanese (ja)
Other versions
JP2008531337A (ja
Filing date
Publication date
Priority claimed from US11/064,824 external-priority patent/US8790485B2/en
Application filed filed Critical
Publication of JP2008531337A publication Critical patent/JP2008531337A/ja
Publication of JP2008531337A5 publication Critical patent/JP2008531337A5/ja
Abandoned legal-status Critical Current

Links

JP2007557158A 2005-02-25 2006-02-24 単一真空減量複合パネルの修復 Abandoned JP2008531337A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US11/064,824 US8790485B2 (en) 2005-02-25 2005-02-25 Single vacuum debulk composite panel repair
PCT/US2006/006427 WO2006093788A1 (en) 2005-02-25 2006-02-24 Single vacuum debulk composite panel repair

Publications (2)

Publication Number Publication Date
JP2008531337A JP2008531337A (ja) 2008-08-14
JP2008531337A5 true JP2008531337A5 (enExample) 2009-01-29

Family

ID=36440881

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2007557158A Abandoned JP2008531337A (ja) 2005-02-25 2006-02-24 単一真空減量複合パネルの修復

Country Status (12)

Country Link
US (2) US8790485B2 (enExample)
EP (1) EP1851039B1 (enExample)
JP (1) JP2008531337A (enExample)
KR (1) KR20080007432A (enExample)
CN (1) CN101128310A (enExample)
AU (1) AU2006218870A1 (enExample)
BR (1) BRPI0607644A2 (enExample)
CA (1) CA2600006C (enExample)
DE (1) DE602006004308D1 (enExample)
MX (1) MX2007010181A (enExample)
RU (1) RU2007135351A (enExample)
WO (1) WO2006093788A1 (enExample)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8790485B2 (en) * 2005-02-25 2014-07-29 Bell Helicopter Textron Inc. Single vacuum debulk composite panel repair
US20160031197A1 (en) * 2005-02-25 2016-02-04 Bell Helicopter Textron Inc. Method of attaching a composite member to a structure
US7927449B2 (en) * 2005-03-29 2011-04-19 Eclipse Investment, Ltd. Sandwiched article for enhancement of a vehicle
GB0707715D0 (en) * 2007-04-20 2007-05-30 Dunne Desmond C Method of coating a surface with sheet moulding compound
CA2705778C (en) * 2007-11-26 2014-01-07 Bell Helicopter Textron Inc. In-situ, multi-stage debulk, compaction, and single stage curing of thick composite repair laminates
WO2009070729A1 (en) * 2007-11-26 2009-06-04 Bell Helicopter Textron Inc. Multi-stage debulk and compaction of thick composite repair laminates
US9302436B2 (en) * 2007-11-26 2016-04-05 Textron Innovations Inc In-situ, multi-stage debulk, compaction, and single stage curing of thick composite repair laminates
CA2741171A1 (en) * 2008-10-29 2010-05-06 Saab Ab Hot drape forming by means of a stiffness controlled vacuum bag
JP5148466B2 (ja) * 2008-12-15 2013-02-20 三菱重工業株式会社 複合材料の修理方法
CA2763181C (en) * 2009-05-29 2015-04-07 Bell Helicopter Textron Inc. Method for cleaning oil soaked bonded panels and laminates
CH701994A1 (de) * 2009-10-08 2011-04-15 Joerg-Ulrich Zowalla Nasslaminierverfahren und Folienschlauch zum Nasslaminieren.
US8986479B2 (en) 2010-09-30 2015-03-24 The Boeing Company Systems and methods for on-aircraft composite repair using double vacuum debulking
US8262841B2 (en) * 2010-11-24 2012-09-11 The Boeing Company Methods for void-free debulking of adhesive bonded joints
EP2632723B1 (en) * 2011-01-11 2016-03-30 Bell Helicopter Textron Inc. Single stage debulk and cure of a prepreg material
CH705257A1 (de) 2011-07-07 2013-01-15 Joerg-Ulrich Zowalla System zur Herstellung und Reparatur von Kunststoff-Composite-Bauteilen.
US20140265058A1 (en) * 2013-03-13 2014-09-18 North Thin Ply Technology Llc System and method for maneuvering thin ply technology complexes
US10357925B2 (en) 2013-12-20 2019-07-23 United Technologies Corporation Enhanced volatile removal for composite layup
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
WO2016118449A1 (en) * 2015-01-20 2016-07-28 Sikorsky Aircraft Corporation Composite repair armature
US10222353B2 (en) * 2015-03-18 2019-03-05 The Boeing Company Method and assembly for inspecting a partially cured repair patch prior to installation
US10589837B2 (en) 2016-02-08 2020-03-17 Bell Helicopter Textron Inc. Spar for a composite wing structure
US10513325B2 (en) 2016-02-08 2019-12-24 Bell Helicopter Textron Inc. Joint member for a composite wing structure
US10836121B2 (en) 2016-02-08 2020-11-17 Bell Helicopter Textron Inc. Methods of manufacture of a composite wing structure
CN105984156A (zh) * 2016-02-14 2016-10-05 芜湖金光汽车配件有限责任公司 一种rtm产品缺陷的修补方法
FR3051135B1 (fr) * 2016-05-10 2019-05-31 Roctool Dispositif et procede pour le moulage et la consolidation d’une preforme textile
EP3566844A4 (en) 2017-03-10 2020-01-08 Mitsubishi Heavy Industries, Ltd. COMPOSITE MATERIAL PRESSURIZING DEVICE AND COMPOSITE MATERIAL FORMING METHOD
US20190030836A1 (en) 2017-07-28 2019-01-31 Airtech International, Inc. Elastic fastener for vacuum bag pleats
US11040496B2 (en) * 2017-12-19 2021-06-22 The Boeing Company Methods and systems for repairing composite structures
US10843413B2 (en) * 2018-03-26 2020-11-24 Textron Innovations Inc. Methods for forming bonded structures
US11230069B2 (en) 2019-08-28 2022-01-25 Textron Innovations Inc. Tool for forming a composite member
US20220016856A1 (en) 2020-07-16 2022-01-20 Honeywell Federal Manufacturing & Technologies, Llc Customized composite debulking caul
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

Family Cites Families (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3993520A (en) 1974-05-06 1976-11-23 Frank D. Werner Windshield repair apparatus and method
US4409048A (en) 1975-03-10 1983-10-11 Hitco High temperature consolidation process
US4357193A (en) * 1979-05-21 1982-11-02 Rockwell International Corporation Method of fabricating a composite structure
US4409270A (en) 1982-04-22 1983-10-11 The General Tire & Rubber Company Method for repairing glass fiber reinforced plastic parts and product
US4659624A (en) 1983-11-25 1987-04-21 Ltv Aerospace & Defense Company Hybrid and unidirectional carbon-carbon fiber reinforced laminate composites
US4554036A (en) 1984-05-07 1985-11-19 Newsom Cosby M Portable vacuum device and method of using same
US4560428A (en) 1984-08-20 1985-12-24 Rockwell International Corporation System and method for producing cured composites
US4820564A (en) 1984-10-29 1989-04-11 The Boeing Company Blind-side repair patch kit
US4652319A (en) 1984-12-03 1987-03-24 Hammond Russell E Method of curing patches on contoured surfaces
US4732639A (en) 1985-08-30 1988-03-22 Newsom Cosby M Vacuum bagging apparatus
US4855182A (en) 1986-10-03 1989-08-08 Isovolta Osterreichische Isolierstoffwerke Aktiengesellschaft Repair laminate
US4769197A (en) 1987-02-02 1988-09-06 United Technologies Corporation Method for molding precured high temperature resins
US4808253A (en) 1987-11-06 1989-02-28 Grumman Aerospace Corporation Method and apparatus for performing a repair on a contoured section of a composite structure
DE69115792T2 (de) 1990-08-20 1996-08-08 Michael D Stewart Raparier-Laminat und Verfahren zur Reparatur einer beschädigten, spannungsfreien Luftschiffstruktur
CA2056330C (en) 1990-12-19 2003-06-10 Alexander C. Dublinski Method of fabricating a complex part made of composite material
US5131834A (en) 1990-12-21 1992-07-21 Northrop Corporation Silicone gel isostatic pressurizing bag and method of use and manufacture
US5116216A (en) 1991-02-28 1992-05-26 The United States Of America As Represented By The Secretary Of The Navy Apparatus for preparing thermoplastic composites
US6270603B1 (en) 1991-04-09 2001-08-07 The Boeing Company Repair method for uniformly heating composite structure
US5442156A (en) 1991-04-09 1995-08-15 The Boeing Company Heating apparatus for composite structure repair
US5374388A (en) 1993-04-22 1994-12-20 Lockheed Corporation Method of forming contoured repair patches
US5595692A (en) 1994-09-13 1997-01-21 United Technologies Corporation Method of repairing resin impregnated articles
US5753271A (en) 1995-08-18 1998-05-19 Northrop Grumman Corporation Heat blanket buffer assembly
US6036464A (en) 1995-08-18 2000-03-14 Northrop Grumman Corporation Heat blanket buffer assembly
US5738741A (en) 1996-03-26 1998-04-14 The University Of Dayton Pre-fabricated vacuum bag and vacuum bag process to externally reinforce structural members with advanced composites
GB9622780D0 (en) 1996-11-01 1997-01-08 British Aerospace Repair of composite laminates
US5958166A (en) 1996-12-31 1999-09-28 Mcdonnell Douglas Corporation Method for repairing high temperature composite structures
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
US6679965B1 (en) 1997-06-04 2004-01-20 Alliant Techsystems Inc. Low density composite rocket nozzle components and process for making the same from standard density phenolic matrix, fiber reinforced materials
US6222007B1 (en) * 1998-05-29 2001-04-24 The United States Of America As Represented By The National Aeronautics And Space Administration Films, preimpregnated tapes and composites made from polyimide “Salt-like” Solutions
US6561247B2 (en) 1998-06-29 2003-05-13 General Electric Company Method and apparatus for repairing a discrete damaged portion of an article surface
US6107976A (en) 1999-03-25 2000-08-22 Bradley B. Teel Hybrid core sandwich radome
CN1224495C (zh) 2000-03-03 2005-10-26 快速科技有限公司 复合材料部件和金属部件的生产、成形、粘接、连接和修理系统
US6385836B1 (en) 2000-06-30 2002-05-14 Lockheed Martin Corporation Method for composite material repair
US6761783B2 (en) 2002-04-09 2004-07-13 The Boeing Company Process method to repair bismaleimide (BMI) composite structures
US6758924B1 (en) 2002-04-15 2004-07-06 The United States Of America As Represented By The Secretary Of The Air Force Method of repairing cracked aircraft structures
US8790485B2 (en) * 2005-02-25 2014-07-29 Bell Helicopter Textron Inc. Single vacuum debulk composite panel repair

Similar Documents

Publication Publication Date Title
JP2008531337A5 (enExample)
RU2007135351A (ru) Ремонт композитной панели с уменьшением объема при использовании одного источника вакуума
RU2011133776A (ru) Способ по меньшей мере частичного восстановления или замены усиливающего элемента конструкции из волокнистого композита и соответствующее соединительное устройство
JP6100579B2 (ja) ハニカムコアサンドイッチパネルの修理方法、および修理装置
JP7093299B2 (ja) 熱プレス装置および金属樹脂複合体の成形方法
CN102950778B (zh) 用于对复合物进行成型和固化的方法和设备
WO2009016552A3 (en) A method of manufacturing a curved element made of composite material
JP6463094B2 (ja) 接合装置及び接合方法
US10322552B2 (en) Composite repair armature
CN203761582U (zh) 一种扬声器震动系统及其运用的扬声器
US9221201B2 (en) Method for manufacturing composite material
CN101801661A (zh) 可再循环复合材料及用于制造其的方法和成套工具
JP6750735B2 (ja) 複合材料の成形方法および複合材料の成形装置
US10507622B2 (en) System and method for curing polymer matrix composite parts in manufacturing and repairing processes
JP5020241B2 (ja) 航空機用サンドイッチ部品をエネルギー効率よく硬化するプレス装置
JP2014237221A (ja) 繊維強化プラスチック部材の成形方法及び成形装置
DE602008006425D1 (de) Mitverklebte druckplatte und verfahren zu deren herstellung
JP2007172929A5 (enExample)
JP2010000655A (ja) ハニカムサンドイッチパネルおよびその製造方法
JP6724667B2 (ja) 複合材料の成形方法および複合材料の成形装置
JP4464208B2 (ja) ハニカムサンドイッチパネルの製造方法
JP2002248694A (ja) 繊維強化複合材料の成形方法
JP2014019024A (ja) 複合材の成形治具及び複合材の成形方法
JP6152037B2 (ja) 繊維強化プラスチックの成形方法
CN103000357A (zh) 一种具有折弯的磁屏蔽结构及其加工方法