JP6181190B2 - 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 - Google Patents
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 Download PDFInfo
- Publication number
- JP6181190B2 JP6181190B2 JP2015535658A JP2015535658A JP6181190B2 JP 6181190 B2 JP6181190 B2 JP 6181190B2 JP 2015535658 A JP2015535658 A JP 2015535658A JP 2015535658 A JP2015535658 A JP 2015535658A JP 6181190 B2 JP6181190 B2 JP 6181190B2
- Authority
- JP
- Japan
- Prior art keywords
- manifold
- bladder
- tool
- bag
- 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.)
- Active
Links
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
- B29C70/446—Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
- B29C33/48—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling
- B29C33/50—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible
- B29C33/505—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles with means for collapsing or disassembling elastic or flexible cores or mandrels, e.g. inflatable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/544—Details of vacuum bags, e.g. materials or shape
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
- B29L2031/3076—Aircrafts
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
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 JP2015535762A5 (enExample) | 2016-07-28 |
| JP6181190B2 true 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)
| 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)
| 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 |
-
2012
- 2012-10-04 US US13/644,587 patent/US9333713B2/en active Active
-
2013
- 2013-08-28 KR KR1020197037219A patent/KR102121217B1/ko active Active
- 2013-08-28 KR KR1020157002888A patent/KR102059227B1/ko active Active
- 2013-08-28 PT PT137667374T patent/PT2903806T/pt unknown
- 2013-08-28 ES ES13766737T patent/ES2791694T3/es active Active
- 2013-08-28 EP EP13766737.4A patent/EP2903806B1/en active Active
- 2013-08-28 CN CN201380052196.2A patent/CN104703782B/zh active Active
- 2013-08-28 CA CA2880926A patent/CA2880926C/en active Active
- 2013-08-28 BR BR112015004435-2A patent/BR112015004435B1/pt active IP Right Grant
- 2013-08-28 WO PCT/US2013/057089 patent/WO2014055180A1/en not_active Ceased
- 2013-08-28 JP JP2015535658A patent/JP6181190B2/ja active Active
-
2016
- 2016-05-09 US US15/150,425 patent/US9738039B2/en active Active
Also Published As
| Publication number | Publication date |
|---|---|
| ES2791694T3 (es) | 2020-11-05 |
| CA2880926A1 (en) | 2014-04-10 |
| JP2015535762A (ja) | 2015-12-17 |
| KR20150063355A (ko) | 2015-06-09 |
| BR112015004435B1 (pt) | 2021-02-02 |
| US9738039B2 (en) | 2017-08-22 |
| PT2903806T (pt) | 2020-04-03 |
| US9333713B2 (en) | 2016-05-10 |
| BR112015004435A2 (pt) | 2017-07-04 |
| KR102121217B1 (ko) | 2020-06-11 |
| KR102059227B1 (ko) | 2019-12-24 |
| CN104703782A (zh) | 2015-06-10 |
| EP2903806B1 (en) | 2020-03-25 |
| US20160250813A1 (en) | 2016-09-01 |
| EP2903806A1 (en) | 2015-08-12 |
| US20140096903A1 (en) | 2014-04-10 |
| KR20190142428A (ko) | 2019-12-26 |
| CA2880926C (en) | 2017-03-28 |
| WO2014055180A1 (en) | 2014-04-10 |
| CN104703782B (zh) | 2017-05-17 |
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