ATE482808T1 - Verfahren und formkern zur herstellung einer faserverbundkomponente für luft- und raumfahrt - Google Patents
Verfahren und formkern zur herstellung einer faserverbundkomponente für luft- und raumfahrtInfo
- Publication number
- ATE482808T1 ATE482808T1 AT07787084T AT07787084T ATE482808T1 AT E482808 T1 ATE482808 T1 AT E482808T1 AT 07787084 T AT07787084 T AT 07787084T AT 07787084 T AT07787084 T AT 07787084T AT E482808 T1 ATE482808 T1 AT E482808T1
- Authority
- AT
- Austria
- Prior art keywords
- layup
- form core
- tubes
- aerospace
- curing
- Prior art date
Links
Classifications
-
- 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
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24628—Nonplanar uniform thickness material
- Y10T428/24661—Forming, or cooperating to form cells
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US81893206P | 2006-07-06 | 2006-07-06 | |
DE102006031334A DE102006031334A1 (de) | 2006-07-06 | 2006-07-06 | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
PCT/EP2007/056788 WO2008003733A1 (en) | 2006-07-06 | 2007-07-05 | Method and moulding core for producing a fibre composite component for aviation and spaceflight and fibre composite component obtained thereby |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE482808T1 true ATE482808T1 (de) | 2010-10-15 |
Family
ID=38806034
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT07787084T ATE482808T1 (de) | 2006-07-06 | 2007-07-05 | Verfahren und formkern zur herstellung einer faserverbundkomponente für luft- und raumfahrt |
Country Status (6)
Country | Link |
---|---|
US (1) | US8906489B2 (de) |
CN (1) | CN101484290B (de) |
AT (1) | ATE482808T1 (de) |
BR (1) | BRPI0714226A2 (de) |
DE (2) | DE102006031334A1 (de) |
RU (1) | RU2438866C2 (de) |
Families Citing this family (38)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006031323B4 (de) * | 2006-07-06 | 2010-07-15 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102006031325B4 (de) | 2006-07-06 | 2010-07-01 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102006031335B4 (de) * | 2006-07-06 | 2011-01-27 | Airbus Operations Gmbh | 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 |
US7879276B2 (en) * | 2007-11-08 | 2011-02-01 | The Boeing Company | Foam stiffened hollow composite stringer |
GB0813161D0 (en) * | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
GB0813146D0 (en) * | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
US8540921B2 (en) | 2008-11-25 | 2013-09-24 | The Boeing Company | Method of forming a reinforced foam-filled composite stringer |
DE102009002697B4 (de) * | 2009-04-28 | 2014-02-27 | Airbus Operations Gmbh | Formkern und Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
US8500066B2 (en) | 2009-06-12 | 2013-08-06 | The Boeing Company | Method and apparatus for wireless aircraft communications and power system using fuselage stringers |
DE102009027049B4 (de) | 2009-06-19 | 2011-09-15 | Cotesa Gmbh | Verfahren zur Integration hohlraumbildender Strukturen in Faserverbundschalen |
US8570152B2 (en) | 2009-07-23 | 2013-10-29 | The Boeing Company | Method and apparatus for wireless sensing with power harvesting of a wireless signal |
US8617687B2 (en) | 2009-08-03 | 2013-12-31 | The Boeing Company | Multi-functional aircraft structures |
DE102009029575B4 (de) | 2009-09-18 | 2011-06-22 | Airbus Operations GmbH, 21129 | Verfahren zur Versteifung eines Faserverbundbauteils und Anordnung zur Herstellung eines versteiften Faserverbundteils |
GB2475523B (en) * | 2009-11-20 | 2012-09-05 | Gkn Aerospace Services Ltd | Dual-skin structures |
DE102010024120B4 (de) | 2010-06-17 | 2014-10-23 | Premium Aerotec Gmbh | Stützprofil |
US20130115429A1 (en) | 2010-07-13 | 2013-05-09 | Learjet | Composite structure and method of forming same |
CN101890807B (zh) * | 2010-07-19 | 2012-10-10 | 哈尔滨飞机工业集团有限责任公司 | 一种利用硅橡胶热膨胀加压成型复合材料零件的方法 |
FR2963273B1 (fr) * | 2010-07-29 | 2014-01-03 | Airbus Operations Sas | Procede de fabrication d'un panneau raidi en materiau composite |
ES2397727B1 (es) * | 2010-10-28 | 2014-01-17 | Airbus Operations, S.L. | Retenedores reutilizables para coencolado de larguerillos no curados. |
JP5773679B2 (ja) | 2011-02-16 | 2015-09-02 | 三菱重工業株式会社 | 炭素繊維強化プラスチック構造体及びその製造方法 |
FR2989310B1 (fr) * | 2012-04-11 | 2014-04-04 | Aircelle Sa | Procede de fabrication d'un panneau sandwich composite a ame alveolaire |
DE102012207950A1 (de) * | 2012-05-11 | 2013-11-14 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils, Stützkern sowie Faserverbundbauteil |
US9308704B2 (en) | 2013-02-18 | 2016-04-12 | The Boeing Company | Elastomeric bladder system |
US10023321B1 (en) * | 2013-06-25 | 2018-07-17 | The Boeing Company | Method and apparatus for forming barriers within cavities |
DE102013020871A1 (de) * | 2013-12-11 | 2015-06-11 | Audi Ag | Strukturbauteil für ein Kraftfahrzeug |
US10293559B2 (en) | 2014-03-04 | 2019-05-21 | Bombardier Inc. | Method and apparatus for forming a composite laminate stack using a breathable polyethylene vacuum film |
EP3131742B1 (de) * | 2014-04-16 | 2023-01-25 | Hexcel Reinforcements SAS | Verfahren zur herstellung eines verbundteils |
DE102014208412A1 (de) * | 2014-05-06 | 2015-11-12 | Bayerische Motoren Werke Aktiengesellschaft | Stützkern und Verfahren zur Herstellung eines faserverstärkten Hohlbauteils |
US9724848B2 (en) * | 2014-07-03 | 2017-08-08 | The Boeing Company | Collapsible, coiled mandrel |
US9701070B2 (en) | 2014-11-06 | 2017-07-11 | Lockheed Martin Corporation | Mandrel forming for discrete wing skin stiffeners |
US20160129985A1 (en) * | 2014-11-08 | 2016-05-12 | Airbus Group India Private Limited | Aircraft structure having cables located in stringers |
GB2533306A (en) * | 2014-12-15 | 2016-06-22 | Airbus Operations Ltd | Sandwich Panel |
DE102015209918A1 (de) * | 2015-05-29 | 2016-12-01 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zur Herstellung eines faserverstärkten Hohlbauteils |
EP3305496B1 (de) * | 2015-06-02 | 2020-07-08 | Mitsubishi Chemical Corporation | Verfahren zur herstellung eines faserverstärkten kunststoffformkörpers |
DE102015117857A1 (de) * | 2015-10-20 | 2017-04-20 | Siempelkamp Maschinen- Und Anlagenbau Gmbh | Verfahren zum Herstellen eines Bauteils aus einem Faserverbundwerkstoff |
US20170232688A1 (en) * | 2016-02-15 | 2017-08-17 | General Electric Company | Incorporation Of Jamming Technologies In Tooling For Composites Processing |
CN107009855A (zh) * | 2017-04-05 | 2017-08-04 | 北京汽车研究总院有限公司 | 一种车门防撞梁及车辆 |
Family Cites Families (93)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2244107A (en) | 1937-10-15 | 1941-06-03 | Hayes Econocrete Corp Of Ameri | Collapsible core |
US3143306A (en) | 1960-08-12 | 1964-08-04 | Preload Corp | Panel making apparatus |
US3279741A (en) | 1965-07-19 | 1966-10-18 | Long Construction Co | Expandable core-former |
US3279739A (en) | 1965-07-19 | 1966-10-18 | Long Construction Co | Expandable core-former |
DE1604528A1 (de) | 1966-06-16 | 1970-11-12 | Bayer Ag | Formkern zur Herstellung von Hohlkoerpern aller Art |
US3551237A (en) | 1967-04-18 | 1970-12-29 | Aerojet General Co | Method of preparing filament-wound open beam structures |
GB1204002A (en) | 1967-11-02 | 1970-09-03 | Ludwig Eigenmann | Process for the continuous production of tubular articles made of textile material in particular for use in lead-acid storage batteries |
US3629030A (en) * | 1968-06-12 | 1971-12-21 | Alvin G Ash | Method for forming a mandrel and fabricating a duct thereabout |
SU433038A1 (ru) | 1971-02-10 | 1974-06-25 | р СПШОБ НЕПРЕРЫВНОГО МЗГО'ЮВЛЕШЯ РЕЗИНОВЫХ РУКАВОВ НА ВЫПЛАВЛЯЕМОМДОРНЕ | |
US3754717A (en) | 1971-07-12 | 1973-08-28 | Dana Corp | Collapsible mandrel |
US3795559A (en) * | 1971-10-01 | 1974-03-05 | Boeing Co | Aircraft fluted core radome and method for making the same |
US3995081A (en) | 1974-10-07 | 1976-11-30 | General Dynamics Corporation | Composite structural beams and method |
US4094688A (en) | 1975-08-21 | 1978-06-13 | Wolf Franz Josef | Method and molding core for making a flexible hollow molded body which is open on a number of sides |
DE2609006B2 (de) | 1976-03-04 | 1979-10-31 | Helios Apparatebau Kg, Mueller & Co, 7220 Schwenningen | Aus faserverstärktem Kunststoff gegossener, hohler Ventilatorflügel |
GB1522432A (en) | 1976-10-21 | 1978-08-23 | Ruggeri V | Method of moulding hollow stiffeners or lightweight laminates or wholly box girdered laminates in fibre reinforced plastics |
US4155970A (en) | 1977-11-04 | 1979-05-22 | Mcdonnell Douglas Corporation | Method for making a hollow composite using a destructible core |
DE2757473A1 (de) | 1977-12-22 | 1979-07-05 | Bayer Ag | Verfahren zum entformen eines auf einem kern aufgebauten kunststoff-formteils |
GB2067455A (en) | 1979-02-20 | 1981-07-30 | Rolls Royce | Composite structure |
JPS5818240A (ja) | 1981-07-28 | 1983-02-02 | Dainichi Nippon Cables Ltd | 狭口容器の製造方法 |
JPS59121172U (ja) | 1983-02-04 | 1984-08-15 | ミネソタ・マイニング・アンド・マニユフアクチユアリング・コンパニ− | ケーブル電線被覆の剥離部分のカバー装置 |
JPS59157807A (ja) | 1983-02-28 | 1984-09-07 | Nec Home Electronics Ltd | ビデオテ−プレコ−ダ |
US4520988A (en) | 1984-04-23 | 1985-06-04 | Harsco Corporation | Concrete core-wall form and stripping assembly therefor |
DE3421364A1 (de) | 1984-06-08 | 1985-12-12 | Bayer Ag, 5090 Leverkusen | Verfahren und vorrichtung zum kontinuierlichen herstellen von laenglichen hohlkoerpern, insbesondere von schlaeuchen, rohren oder innenlinern fuer solche, aus einem fluessigen material, wie reaktionsgemisch oder schmelze |
JPS61188425A (ja) | 1985-02-18 | 1986-08-22 | Toyota Motor Corp | 摩擦材の製造方法 |
DE3670788D1 (de) | 1985-08-22 | 1990-06-07 | Budd Co | Verfahren zur herstellung eines hohlen faserverstaerkten gegenstandes. |
US4943334A (en) | 1986-09-15 | 1990-07-24 | Compositech Ltd. | Method for making reinforced plastic laminates for use in the production of circuit boards |
DE3715915A1 (de) | 1987-05-13 | 1988-12-08 | Minnesota Mining & Mfg | Stuetzwendel fuer einen radial gedehnten huelsenkoerper |
US5045251A (en) | 1987-06-15 | 1991-09-03 | Ford Motor Company | Method of resin transfer molding a composite article |
DE8711336U1 (de) | 1987-08-20 | 1987-10-22 | Ems-Inventa Ag, Zuerich, Ch | |
DD277234A1 (de) | 1988-11-21 | 1990-03-28 | Staaken Plastverarbeitung | Vorrichtung zur herstellung von rohren aus glasfaserverstaerkten ungesaettigten kunstharzen |
JPH0722977B2 (ja) | 1989-03-22 | 1995-03-15 | 三ツ星ベルト株式会社 | ローエッジベルトの製造方法および成形型 |
DE3911312C1 (en) | 1989-04-07 | 1990-04-19 | Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De | Mould core (former) for winding a fibre-reinforced body of plastic |
US5041315A (en) | 1989-05-15 | 1991-08-20 | Zircoa Inc. | Flexible ceramic member and method of production thereof |
US5176864A (en) | 1989-06-12 | 1993-01-05 | Aluminum Company Of America | Lost wax process utilizing a high temperature wax-based material |
JPH03277532A (ja) | 1990-03-28 | 1991-12-09 | Nippon Steel Chem Co Ltd | 繊維強化プラスチック曲管の製造方法 |
CA2056224A1 (en) | 1990-12-19 | 1992-06-20 | Terry Martin Boustead | Conformal composite molding |
JPH0767704B2 (ja) | 1991-02-21 | 1995-07-26 | 川崎重工業株式会社 | 中空複合部材の製造方法 |
US5262121A (en) | 1991-12-18 | 1993-11-16 | Goodno Kenneth T | Method of making and using flexible mandrel |
US5387098A (en) | 1992-04-23 | 1995-02-07 | The Boeing Company | Flexible reusable mandrels |
DE4224526A1 (de) | 1992-07-24 | 1994-01-27 | Siemens Ag | Kaltschrumpf-Schlauch |
JPH06106632A (ja) | 1992-09-30 | 1994-04-19 | Sakura Rubber Kk | 複合材製品の成形方法 |
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 |
GB2284173A (en) | 1993-02-06 | 1995-05-31 | Alan Harper | Collapsible core tool for lost-core moulding |
RU2143341C1 (ru) | 1993-07-21 | 1999-12-27 | Э.Хашогги Индастриз | Изделие, изготовленное из неорганически наполненного материала, способ его изготовления и устройство для его осуществления (варианты) |
WO1995014563A1 (en) | 1993-11-26 | 1995-06-01 | Alan Roger Harper | Casting method and apparatus and products thereof |
US5505492A (en) | 1994-02-09 | 1996-04-09 | Radius Engineering, Inc. | Composite pole and manufacturing process for composite poles of varying non-circular cross-sections and curved center lines |
GB2292332B (en) | 1994-04-22 | 1999-04-28 | Alan Roger Harper | Moulding process and apparatus therefor |
JPH08142060A (ja) | 1994-11-21 | 1996-06-04 | Sumino Kogyo Kk | 中子の製造方法とその中子及び成形金型 |
JP2951561B2 (ja) | 1995-01-27 | 1999-09-20 | 太陽誘電株式会社 | 電子機器用コイル部品 |
JP2640338B2 (ja) | 1995-02-02 | 1997-08-13 | 富士夫 坂本 | 成型金型および成型方法 |
IT1275976B1 (it) | 1995-03-27 | 1997-10-24 | Pirelli Cavi S P A Ora Pirelli | Supporto per un manicotto elastico |
US6013125A (en) | 1995-09-13 | 2000-01-11 | Quraishi; Mashallah M. | Investment of powders and method for rapid preparation of investment molds |
US5931830A (en) | 1995-12-07 | 1999-08-03 | Sarcos L.C. | Hollow coil guide wire apparatus for catheters |
FR2745745B1 (fr) | 1996-03-07 | 1998-04-10 | Snecma | Procede de fabrication d'une piece en materiau composite comportant une cavite revetue d'une protection de surface |
US5989481A (en) | 1996-06-18 | 1999-11-23 | You; Daniel H. | Golf club shaft manufacturing process |
US6692681B1 (en) | 1997-01-29 | 2004-02-17 | Raytheon Aircraft Company | Method and apparatus for manufacturing composite structures |
US6340509B1 (en) | 1997-04-23 | 2002-01-22 | Radius Engineering, Inc. | Composite bicycle frame and method of construction thereof |
JPH1190979A (ja) | 1997-09-19 | 1999-04-06 | Tokai Rubber Ind Ltd | 曲形ホースの製造方法 |
CA2253037C (en) | 1997-11-12 | 2004-11-02 | Sakura Rubber Co., Ltd. | Method of manufacturing structure by using biodegradable mold |
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 |
ES2194479T5 (es) | 1998-07-03 | 2014-02-04 | Siemens Aktiengesellschaft | Procedimiento para fabricar estructuras compuestas cerradas y aparato de moldeo a utilizar con dicho procedimiento |
US6889937B2 (en) | 1999-11-18 | 2005-05-10 | Rocky Mountain Composites, Inc. | Single piece co-cure composite wing |
DE60018455T3 (de) | 1999-12-07 | 2009-02-19 | The Boeing Company, Seattle | Doppelfolien vakuuminjektionsverfahren zur herstellung eines verbundwerkstoffes und damit hergestellter verbundwerkstoff |
CN2400258Y (zh) * | 2000-01-12 | 2000-10-11 | 洪进山 | 复合材料成型模具 |
AU2001262912A1 (en) | 2000-02-25 | 2001-09-03 | The Boeing Company | Laminated composite radius filler |
DE10013409C1 (de) | 2000-03-17 | 2000-11-23 | Daimler Chrysler Ag | Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens |
EP1190828A1 (de) | 2000-09-26 | 2002-03-27 | Recticel | Form und Verfahren zum Herstellen von Polyurethangegenständen |
EP1197309B1 (de) | 2000-10-04 | 2004-04-07 | Alcan Technology & Management AG | Verfahren zur Herstellung von Bauteilen aus Faserverbundkunststoffen |
WO2002040254A2 (en) | 2000-11-15 | 2002-05-23 | Toyota Motor Sales, U.S.A., Inc. | One-piece closed-shape structure and method of forming same |
US6638466B1 (en) | 2000-12-28 | 2003-10-28 | Raytheon Aircraft Company | Methods of manufacturing separable structures |
JP4721251B2 (ja) | 2001-09-03 | 2011-07-13 | 富士重工業株式会社 | 複合材補強板の製造方法 |
JP4690613B2 (ja) | 2001-09-28 | 2011-06-01 | 富士重工業株式会社 | 複合材製中空体の製造方法 |
US7344670B2 (en) | 2002-03-28 | 2008-03-18 | Build A Mold Limited | Lost core plastic molding process for transferring, positioning and molding inserts into a plastic part |
US7559332B2 (en) | 2002-07-02 | 2009-07-14 | Toyota Motor Sales U.S.A., Inc. | Media removal apparatus and methods of removing media |
US7217380B2 (en) | 2002-07-22 | 2007-05-15 | Toyota Motor Sales, Usa, Inc. | Vibration apparatus and methods of vibration |
US7204951B2 (en) | 2002-07-30 | 2007-04-17 | Rocky Mountain Composites, Inc. | Method of assembling a single piece co-cured structure |
US7101453B2 (en) | 2002-09-04 | 2006-09-05 | Toyota Motor Sales U.S.A., Inc. | Pre-filled contained media volumes and methods of media filling using pre-filled contained media volumes |
RU2242369C1 (ru) | 2003-05-19 | 2004-12-20 | Федеральное государственное унитарное предприятие "Обнинское научно-производственное предприятие "Технология" | Опорный узел трехслойной панели |
DE10342867B4 (de) | 2003-09-15 | 2008-05-29 | Eurocopter Deutschland Gmbh | Verfahren zur Herstellung eines wasserlöslichen Formkerns |
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 |
US7293737B2 (en) * | 2004-04-20 | 2007-11-13 | The Boeing Company | Co-cured stringers and associated mandrel and fabrication method |
US7531058B2 (en) | 2005-02-24 | 2009-05-12 | The Boeing Company | Reinforced rampdown for composite structural member and method for same |
RU2285613C1 (ru) | 2005-05-18 | 2006-10-20 | Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") | Способ изготовления многослойного изделия из полимерных композиционных материалов |
US7824171B2 (en) * | 2005-10-31 | 2010-11-02 | The Boeing Company | Corner-consolidating inflatable apparatus and method for manufacturing composite structures |
US7633040B2 (en) | 2005-11-14 | 2009-12-15 | The Boeing Company | Bulk resin infusion system apparatus and method |
FR2898539B1 (fr) | 2006-03-20 | 2008-05-23 | Eads Ccr Groupement D Interet | Procede de realisation de panneaux raidis en materiau composite et panneaux ainsi realises |
DE102006031335B4 (de) | 2006-07-06 | 2011-01-27 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102006031326B4 (de) | 2006-07-06 | 2010-09-23 | Airbus Deutschland Gmbh | Formkern und Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102006031325B4 (de) | 2006-07-06 | 2010-07-01 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
EP2038100B1 (de) | 2006-07-06 | 2010-09-29 | Airbus Deutschland GmbH | Verfahren und formkern zur herstellung einer faserverbundkomponente für luft- und raumfahrt |
DE102006031336B4 (de) | 2006-07-06 | 2010-08-05 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils in der Luft- und Raumfahrt |
DE102006031323B4 (de) | 2006-07-06 | 2010-07-15 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt |
DE102009023835B4 (de) | 2009-06-04 | 2011-02-10 | Schmitz-Werke Gmbh + Co Kg | Befestigungs-Vorrichtung |
-
2006
- 2006-07-06 DE DE102006031334A patent/DE102006031334A1/de not_active Ceased
-
2007
- 2007-07-05 CN CN2007800256355A patent/CN101484290B/zh active Active
- 2007-07-05 RU RU2009103204/05A patent/RU2438866C2/ru not_active IP Right Cessation
- 2007-07-05 US US12/308,792 patent/US8906489B2/en active Active
- 2007-07-05 AT AT07787084T patent/ATE482808T1/de not_active IP Right Cessation
- 2007-07-05 BR BRPI0714226-9A2A patent/BRPI0714226A2/pt not_active IP Right Cessation
- 2007-07-05 DE DE602007009529T patent/DE602007009529D1/de active Active
Also Published As
Publication number | Publication date |
---|---|
DE102006031334A1 (de) | 2008-01-10 |
CN101484290A (zh) | 2009-07-15 |
CN101484290B (zh) | 2012-06-27 |
US20110076461A1 (en) | 2011-03-31 |
DE602007009529D1 (de) | 2010-11-11 |
RU2438866C2 (ru) | 2012-01-10 |
RU2009103204A (ru) | 2010-08-20 |
BRPI0714226A2 (pt) | 2013-10-29 |
US8906489B2 (en) | 2014-12-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ATE482808T1 (de) | Verfahren und formkern zur herstellung einer faserverbundkomponente für luft- und raumfahrt | |
ATE454260T1 (de) | Verfahren zur herstellung einer faserverbundkomponente für flugzeuge und raumschiffe | |
EP2516140B1 (de) | Verfahren zur herstellung einer verbundschalenstruktur | |
US9517613B2 (en) | Method of forming a composite structure comprising a flange | |
EP2318198B1 (de) | Zusammenfügen und formen einer verbundschichtplatte und vorrichtung dafür | |
US10100165B2 (en) | Silicone-coated release film with a special vacuum deep drawing capability | |
EP2723554A2 (de) | Werkzeug zur herstellung einer vorformanordnung | |
EP2953786B1 (de) | Verfahren und vorrichtung zur überarbeitung von strukturen | |
EP2043832B8 (de) | Verfahren zur herstellung einer faserverbundkomponente unter verwendung eines formkerns und formkern | |
US20080210372A1 (en) | Composite article debulking process | |
ATE553911T1 (de) | Verfahren zur versteifung eines faserverbundbauteils sowie vakuummatte und anordnung zur herstellung eines versteiften faserverbundbauteils | |
WO2009115736A3 (fr) | Procédé et dispositif de moulage d'une pièce courbe en matériau composite, et pièce correspondante | |
ATE539874T1 (de) | Verfahren zur herstellung eines profils aus faserverbundwerkstoff | |
DE602007008560D1 (de) | Vakuumiervorgang zur Verwendung bei einem Verfahren zur Herstellung einer Verbundstruktur | |
AU2015200414A1 (en) | Fabrication of composite laminates using temporarily stitched preforms | |
JP5315147B2 (ja) | 中空構造用プリプレグ成形体の成形方法及び複合材成形品の成形方法 | |
CN102756481A (zh) | 风机叶片用碳纤维大梁的制作方法 | |
DE602006010207D1 (de) | Verfahren zur herstellung von flugzeugsperren aus verbundmaterial aus kohlenstoff | |
CN104441693A (zh) | 一种风力发电叶片新型复合材料胶膜成型工艺方法 | |
EP2889126B1 (de) | Verfahren zum herstellen einer verbundstoffmaterialform für ein langes element aus verbundstoffmaterial | |
CN107073844B (zh) | 模塑材料以及形成其的方法 | |
JP2012040689A (ja) | 繊維強化複合材料の製造方法 | |
Bonnemains et al. | Preform influence on mechanical behavior of stiffened panels manufactured by liquid resin infusion | |
JPH04268342A (ja) | 炭素繊維強化複合材料の作製方法 | |
KOYAMA et al. | Effect of Curved Mold for Thermal Deformation of CFRP Laminates |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |