JP2015535762A5 - - Google Patents

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Publication number
JP2015535762A5
JP2015535762A5 JP2015535658A JP2015535658A JP2015535762A5 JP 2015535762 A5 JP2015535762 A5 JP 2015535762A5 JP 2015535658 A JP2015535658 A JP 2015535658A JP 2015535658 A JP2015535658 A JP 2015535658A JP 2015535762 A5 JP2015535762 A5 JP 2015535762A5
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JP
Japan
Prior art keywords
manifold
bag
bladder
tool
stiffener
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
JP2015535658A
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English (en)
Japanese (ja)
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JP2015535762A (ja
JP6181190B2 (ja
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Publication date
Priority claimed from US13/644,587 external-priority patent/US9333713B2/en
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Publication of JP2015535762A publication Critical patent/JP2015535762A/ja
Publication of JP2015535762A5 publication Critical patent/JP2015535762A5/ja
Application granted granted Critical
Publication of JP6181190B2 publication Critical patent/JP6181190B2/ja
Active legal-status Critical Current
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JP2015535658A 2012-10-04 2013-08-28 複合材外板と複合材スティフナとをオートクレーブ内で共硬化するための方法及び装置 Active JP6181190B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/644,587 US9333713B2 (en) 2012-10-04 2012-10-04 Method for co-curing composite skins and stiffeners in an autoclave
US13/644,587 2012-10-04
PCT/US2013/057089 WO2014055180A1 (en) 2012-10-04 2013-08-28 Method and apparatus for co-curing composite skins and stiffeners in an autoclave

Publications (3)

Publication Number Publication Date
JP2015535762A JP2015535762A (ja) 2015-12-17
JP2015535762A5 true JP2015535762A5 (enExample) 2016-07-28
JP6181190B2 JP6181190B2 (ja) 2017-08-16

Family

ID=49237591

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015535658A Active JP6181190B2 (ja) 2012-10-04 2013-08-28 複合材外板と複合材スティフナとをオートクレーブ内で共硬化するための方法及び装置

Country Status (10)

Country Link
US (2) US9333713B2 (enExample)
EP (1) EP2903806B1 (enExample)
JP (1) JP6181190B2 (enExample)
KR (2) KR102121217B1 (enExample)
CN (1) CN104703782B (enExample)
BR (1) BR112015004435B1 (enExample)
CA (1) CA2880926C (enExample)
ES (1) ES2791694T3 (enExample)
PT (1) PT2903806T (enExample)
WO (1) WO2014055180A1 (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9333713B2 (en) 2012-10-04 2016-05-10 The Boeing Company Method for co-curing composite skins and stiffeners in an autoclave
US9914244B2 (en) * 2014-08-04 2018-03-13 The Boeing Company Bladder system for curing composite parts
US9862122B2 (en) * 2014-08-14 2018-01-09 The Boeing Company Reinforced bladder
US10751955B2 (en) * 2017-04-10 2020-08-25 The Boeing Company Unitized composite structure manufacturing system
EP3999162A1 (en) * 2019-07-19 2022-05-25 C.R. Bard, Inc. Lamination apparatus for medical balloons and related methods
US11559954B2 (en) * 2020-01-16 2023-01-24 The Boeing Company Multi-chamber conformable bladder for composite part tooling
CN111452395B (zh) * 2020-03-26 2021-11-12 中车青岛四方机车车辆股份有限公司 曲面复合材料连接结构、成型方法及轨道车辆
CN115195152A (zh) * 2021-04-14 2022-10-18 波音公司 用于处理复合结构的设备和方法
US12379059B2 (en) * 2022-02-07 2025-08-05 The Boeing Company Quick connect manifold for flowable material delivery to a part-forming fixture and associated systems and methods
CN119261233A (zh) * 2024-12-06 2025-01-07 北京玻钢院复合材料有限公司 一种固体火箭发动机绝热层结构的制备方法

Family Cites Families (94)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2485898A (en) 1944-06-20 1949-10-25 Charles B Mathews Inflatable core for use in casting hollow concrete units
US3306767A (en) 1962-09-20 1967-02-28 Boeing Co Method of applying a resin laminar substrate to a surface
US3610563A (en) 1969-08-20 1971-10-05 Structural Fibers Mandrel for forming fiber-reinforced plastic articles
US3700512A (en) 1969-09-05 1972-10-24 Owens Corning Fiberglass Corp Method of forming a fluid retaining wall
US3764641A (en) 1971-01-08 1973-10-09 A Ash Method of forming irregularly shaped hollow articles using a variable stiffness mandrel
US3768769A (en) 1971-03-29 1973-10-30 C Sachs Pneumatic means for production of molded structures
US3795559A (en) 1971-10-01 1974-03-05 Boeing Co Aircraft fluted core radome and method for making the same
US4087502A (en) 1976-03-24 1978-05-02 Tre Corporation Method of making a collapsible foam mandrel
US4662587A (en) 1981-09-30 1987-05-05 The Boeing Company Composite for aircraft wing and method of making
JPS5856824A (ja) * 1981-09-30 1983-04-04 Kawasaki Heavy Ind Ltd 複合材桁構造物製造方法
US4675061A (en) 1985-09-24 1987-06-23 Grumman Aerospace Corporation Method for forming corrugated materials using memory metal cores
US4780262A (en) 1986-01-15 1988-10-25 The Boeing Company Method for making composite structures
JPS62186055A (ja) * 1986-02-12 1987-08-14 Sanshin Ind Co Ltd 燃料噴射機関の噴射ポンプ駆動構造
US4681724A (en) 1986-04-28 1987-07-21 United Technologies Corporation Removable irreversibly shrinking male mandrel
EP0254901A3 (en) * 1986-07-18 1990-05-23 Tektronix, Inc. Lamination method and apparatus
US4946526A (en) 1987-10-29 1990-08-07 Ltv Aerospace And Defense Company Method for compression molding of laminated panels
IT1223923B (it) 1988-11-22 1990-09-29 Ferrari Engineering Spa Procedimento per la costruzione di elementi monolitici cavi in materiale composito in particolare in fibra di carbonio
US5484277A (en) 1989-12-26 1996-01-16 Mcdonnell Douglas Corporation Mandreless molding system
US5397524A (en) 1991-05-06 1995-03-14 Godonco Industries, Inc. Apparatus and method for manufacturing concrete form mouldings
US5106568A (en) 1991-11-15 1992-04-21 Mcdonnell Douglas Corporation Method and apparatus for vacuum bag molding of composite materials
FR2685249B1 (fr) 1991-12-24 1994-02-11 Snecma Procede de fabrication d'une pale de soufflante en materiau composite et outillage de moulage.
US5387098A (en) 1992-04-23 1995-02-07 The Boeing Company Flexible reusable mandrels
US5259901A (en) 1992-05-27 1993-11-09 Thiokol Corporation Method for constructing an inflatable mandrel
US5290121A (en) 1992-05-28 1994-03-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration System for the installation and replacement of components in hostile environments
JPH0671654A (ja) 1992-08-27 1994-03-15 Yokohama Rubber Co Ltd:The 樹脂マンドレル
US5266137A (en) 1992-11-10 1993-11-30 Hollingsworth Ritch D Rigid segmented mandrel with inflatable support
US5354195A (en) 1992-12-23 1994-10-11 United Technologies Corporation Composite molding apparatus for high pressure co-cure molding of lightweight honeycomb core composite articles having ramped surfaces utilizing low density, stabilized ramped honeycomb cores
US5366684A (en) * 1992-12-31 1994-11-22 Grumman Aerospace Corporation Molding composite method using an inflatable bladder pressurized in an autoclave
US5425628A (en) 1993-09-20 1995-06-20 The Boeing Company Pressure bag for tool core
US5469686A (en) 1993-09-27 1995-11-28 Rockwell International Corp. Composite structural truss element
US5451377A (en) * 1993-09-29 1995-09-19 Rockwell International Corp. Composite structures and methods of manufacturing such structures
US5897818A (en) 1994-01-14 1999-04-27 Compsys, Inc. Method for continuously manufacturing a composite preform
US5538589A (en) 1994-08-31 1996-07-23 The Boeing Company Composite stringer assembly machine
US5622733A (en) 1994-10-04 1997-04-22 Rockwell International Corporation Tooling for the fabrication of composite hollow crown-stiffened skins and panels
US5580416A (en) 1994-12-12 1996-12-03 Industrial Technology Research Institute Mandrel assembly
GB2296273B (en) 1994-12-22 1997-03-19 Sofitech Nv Inflatable packers
US5507341A (en) 1994-12-22 1996-04-16 Dowell, A Division Of Schlumberger Technology Corp. Inflatable packer with bladder shape control
US5817269A (en) 1996-10-25 1998-10-06 The Boeing Company Composite fabrication method and tooling to improve part consolidation
US6692681B1 (en) * 1997-01-29 2004-02-17 Raytheon Aircraft Company Method and apparatus for manufacturing composite structures
SE509503C2 (sv) 1997-05-12 1999-02-01 Volvo Ab Arrangemang, förfarande och hålkropp vid formning av plastdetaljer
FR2766407B1 (fr) 1997-07-22 1999-10-15 Aerospatiale Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs
US6458309B1 (en) 1998-06-01 2002-10-01 Rohr, Inc. Method for fabricating an advanced composite aerostructure article having an integral co-cured fly away hollow mandrel
JP2000094623A (ja) * 1998-09-25 2000-04-04 Matsushita Electric Works Ltd 積層体の製造方法
US6510961B1 (en) 1999-04-14 2003-01-28 A&P Technology Integrally-reinforced braided tubular structure and method of producing the same
JP4187878B2 (ja) * 1999-07-19 2008-11-26 富士重工業株式会社 航空機の複合材翼およびその製造方法
US6889937B2 (en) 1999-11-18 2005-05-10 Rocky Mountain Composites, Inc. Single piece co-cure composite wing
FR2808472B1 (fr) 2000-05-05 2003-02-28 Aerospatiale Matra Airbus Procede de fabrication d'un panneau en materiau composite a bandes raidisseurs et panneau ainsi obtenu
JP4526698B2 (ja) 2000-12-22 2010-08-18 富士重工業株式会社 複合材成形品及びその製造方法
US6743504B1 (en) 2001-03-01 2004-06-01 Rohr, Inc. Co-cured composite structures and method of making them
US6497190B1 (en) 2001-05-29 2002-12-24 Compsys, Inc. Conformable composite structural member and method therefor
US7052572B2 (en) 2001-08-01 2006-05-30 Fuji Jukogyo Kabushiki Kaisha Method for manufacturing a structure
US6749171B2 (en) 2001-08-03 2004-06-15 Fukuvi Usa, Inc. Rustication
US7204951B2 (en) 2002-07-30 2007-04-17 Rocky Mountain Composites, Inc. Method of assembling a single piece co-cured structure
US8211530B2 (en) 2003-02-03 2012-07-03 Northrop Grumman Systems Corporation Adhesive fillets and method and apparatus for making same
US7083698B2 (en) 2003-08-22 2006-08-01 The Boeing Company Automated composite lay-up to an internal fuselage mandrel
US7138031B2 (en) 2003-09-09 2006-11-21 The Boeing Company Mandrel and method for manufacturing composite structures
US7294220B2 (en) 2003-10-16 2007-11-13 Toyota Motor Sales, U.S.A., Inc. Methods of stabilizing and/or sealing core material and stabilized and/or sealed core material
US7527222B2 (en) 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7293737B2 (en) 2004-04-20 2007-11-13 The Boeing Company Co-cured stringers and associated mandrel and fabrication method
US7338703B2 (en) 2004-11-24 2008-03-04 Touchstone Research Laboratory, Ltd. Metallic-polymeric composite materials
US7357166B2 (en) 2004-11-24 2008-04-15 The Boeing Company Flexible mandrel for highly contoured composite stringer
US7824171B2 (en) 2005-10-31 2010-11-02 The Boeing Company Corner-consolidating inflatable apparatus and method for manufacturing composite structures
JP4928115B2 (ja) * 2005-11-08 2012-05-09 富士重工業株式会社 成形方法及び成形治具
US7459048B2 (en) 2006-01-31 2008-12-02 The Boeing Company One-piece inner shell for full barrel composite fuselage
WO2007113345A1 (es) 2006-03-31 2007-10-11 Airbus España, S.L. Procedimiento de fabricacion de estructuras de material compuesto con un utillaje colapsable
CN101448626B (zh) 2006-03-31 2012-02-22 空中客车西班牙运营有限责任公司 用可收缩模具制造复合材料结构的方法
US7815160B2 (en) 2006-04-04 2010-10-19 A & P Technology Composite mandrel
US7419130B2 (en) 2006-05-15 2008-09-02 Peery Bros. Lumber Co. Inc. Rustication for architectural molding
WO2008003733A1 (en) 2006-07-06 2008-01-10 Airbus Deutschland Gmbh Method and moulding core for producing a fibre composite component for aviation and spaceflight and fibre composite component obtained thereby
DE102006031326B4 (de) 2006-07-06 2010-09-23 Airbus Deutschland Gmbh Formkern und Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
DE102006031336B4 (de) 2006-07-06 2010-08-05 Airbus Deutschland Gmbh Verfahren zur Herstellung eines Faserverbundbauteils in der Luft- und Raumfahrt
US7854874B2 (en) 2006-11-20 2010-12-21 The Boeing Company Apparatus and methods for forming hat stiffened composite parts using thermally expansive tooling cauls
US20080131716A1 (en) 2006-12-04 2008-06-05 American Consulting Technology & Research, Inc. Shrinkable film barrier for mandrel tooling members
US8691037B2 (en) 2006-12-14 2014-04-08 The Boeing Company Method for minimizing fiber distortion during fabrication of one-piece composite barrel section
US20080277531A1 (en) 2007-05-11 2008-11-13 The Boeing Company Hybrid Composite Panel Systems and Methods
US7861969B2 (en) 2007-05-24 2011-01-04 The Boeing Company Shaped composite stringers and methods of making
US20080302912A1 (en) 2007-06-08 2008-12-11 The Boeing Company Bladderless Mold Line Conformal Hat Stringer
US7879276B2 (en) 2007-11-08 2011-02-01 The Boeing Company Foam stiffened hollow composite stringer
US7897225B2 (en) 2008-02-19 2011-03-01 Composite Technology Development, Inc. Deformable sandwich panel
US9090028B2 (en) * 2008-04-17 2015-07-28 The Boeing Company Method for producing contoured composite structures and structures produced thereby
JP2009292054A (ja) * 2008-06-05 2009-12-17 Motoyasu Hibi 繊維強化プラスチックのプレス成形法
US9238335B2 (en) 2008-07-10 2016-01-19 The Boeing Company Mandrel for autoclave curing applications
US9327467B2 (en) 2008-07-10 2016-05-03 The Boeing Company Composite mandrel for autoclave curing applications
US7998299B2 (en) 2008-10-01 2011-08-16 The Boeing Company Method for making composite truss panel having a fluted core
US20100122763A1 (en) * 2008-11-14 2010-05-20 Iq Tec Switzerland Gmbh Composites and Methods of Making the Same
US8540921B2 (en) 2008-11-25 2013-09-24 The Boeing Company Method of forming a reinforced foam-filled composite stringer
US9296187B2 (en) 2008-12-10 2016-03-29 The Boeing Company Bagging process and mandrel for fabrication of elongated composite structure
US8293051B2 (en) 2008-12-10 2012-10-23 The Boeing Company Method for producing composite laminates using a collapsible mandrel
CN101764289B (zh) * 2008-12-25 2013-09-11 西安飞机工业(集团)有限责任公司 一种金属丝的铺设方法
US20100186899A1 (en) * 2009-01-15 2010-07-29 Airtech International, Inc. Thermoplastic mandrels for composite fabrication
US8074694B2 (en) 2009-05-28 2011-12-13 The Boeing Company Stringer transition method
DE102010024120B4 (de) 2010-06-17 2014-10-23 Premium Aerotec Gmbh Stützprofil
CN102114706B (zh) 2010-12-29 2013-02-13 江西昌河航空工业有限公司 一种复合材料部件框、梁和蒙皮整体共固化成型方法
US9333713B2 (en) 2012-10-04 2016-05-10 The Boeing Company Method for co-curing composite skins and stiffeners in an autoclave

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