WO2009115734A3 - Procede et dispositif de realisation d'un profil courbe en materiau composite, et profil correspondant - Google Patents
Procede et dispositif de realisation d'un profil courbe en materiau composite, et profil correspondant Download PDFInfo
- Publication number
- WO2009115734A3 WO2009115734A3 PCT/FR2009/050357 FR2009050357W WO2009115734A3 WO 2009115734 A3 WO2009115734 A3 WO 2009115734A3 FR 2009050357 W FR2009050357 W FR 2009050357W WO 2009115734 A3 WO2009115734 A3 WO 2009115734A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- section
- band
- producing
- composite material
- resulting
- Prior art date
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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
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
- B29C70/205—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres the structure being shaped to form a three-dimensional configuration
- B29C70/207—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres the structure being shaped to form a three-dimensional configuration arranged in parallel planes of fibres crossing at substantial angles
-
- 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
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
- B29C70/202—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC]
-
- 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
- B29C70/342—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 using isostatic pressure
-
- 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
- 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
- B29D99/0003—Producing profiled members, e.g. beams
-
- 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
- B29L2031/001—Profiled members, e.g. beams, sections
- B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
-
- 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
- B29L2031/3082—Fuselages
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/17—Surface bonding means and/or assemblymeans with work feeding or handling means
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49801—Shaping fiber or fibered material
-
- 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.]
- Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
- Y10T428/24074—Strand or strand-portions
-
- 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.]
- Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
- Y10T428/24074—Strand or strand-portions
- Y10T428/24116—Oblique to direction of web
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Textile Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
Abstract
II s'agit d'un procédé, d'un dispositif pour la réalisation et d'un profil (63) en matériau composite courbe, à partir d'au moins une bande composite (11) s' étendant le long d'un axe longitudinal. La bande est formée par l'empilage d'au moins deux nappes en fibres de renfort (4, 5, 6) unidirectionnelles disposées selon des orientations. On drape la bande sur un gabarit (34, 73) présentant une face d'application (36) plane ou sensiblement plane de forme générale allongée, de configuration déterminée correspondant à celle du profil recherché et s' étendant autour d'une ligne de référence, en appliquant progressivement la bande et en la déformant simultanément selon ladite ligne de référence, de sorte qu'on réalise sur la ou les parties ayant un rayon de courbure non nul un épanouissement progressif des fibres dans le plan d' application.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/920,922 US20110086199A1 (en) | 2008-03-07 | 2009-03-05 | Method and device for producing a curved profile made from composite material and resulting profile |
EP09722505A EP2262634A2 (fr) | 2008-03-07 | 2009-03-05 | Procédé et dispositif de réalisation d'un profil courbe en matériau composite, et profil correspondant |
CN200980113385.XA CN102006986B (zh) | 2008-03-07 | 2009-03-05 | 用于制造由复合材料制成的弯曲型件的方法和设备及制成的型件 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0801261 | 2008-03-07 | ||
FR0801261A FR2928294B1 (fr) | 2008-03-07 | 2008-03-07 | Procede et dispositif de realisation d'un profil courbe en materiau composite,et profil correspondant. |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2009115734A2 WO2009115734A2 (fr) | 2009-09-24 |
WO2009115734A3 true WO2009115734A3 (fr) | 2010-07-29 |
Family
ID=39926474
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR2009/050357 WO2009115734A2 (fr) | 2008-03-07 | 2009-03-05 | Procede et dispositif de realisation d'un profil courbe en materiau composite, et profil correspondant |
Country Status (5)
Country | Link |
---|---|
US (1) | US20110086199A1 (fr) |
EP (1) | EP2262634A2 (fr) |
CN (1) | CN102006986B (fr) |
FR (1) | FR2928294B1 (fr) |
WO (1) | WO2009115734A2 (fr) |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2933423B1 (fr) * | 2008-07-04 | 2010-09-17 | Messier Dowty Sa | Procede de fabrication d'une piece metallique renforcee de fibres ceramiques |
US9266279B2 (en) | 2010-07-08 | 2016-02-23 | Orbital Atk, Inc. | Variable material stretch-forming apparatus and methods |
GB201013524D0 (en) | 2010-08-12 | 2010-09-29 | Hexcel Composites Ltd | Improved composite materials |
FR2965748B1 (fr) * | 2010-10-06 | 2012-10-26 | Coriolis Composites Attn Olivier Bouroullec | Procede de fabrication de raidisseurs en materiau composite |
DE102011002906B4 (de) | 2011-01-20 | 2012-11-29 | Cotesa Gmbh | Umformkern und Verfahren zur Drapierung unidirektionaler 0°-Faserschichten |
ES2400131B1 (es) * | 2011-05-27 | 2014-04-29 | Airbus Operations S.L. | Metodo de apilado para componentes no planos de material compuesto |
FR2977826B1 (fr) * | 2011-07-11 | 2017-01-13 | Airbus Operations Sas | Procede de realisation d'un panneau avec une double courbure |
AT511885B1 (de) * | 2011-08-19 | 2015-05-15 | C6 Gmbh | Verfahren zur herstellung eines bauteils aus einem vorimprägnierten verbundmaterial, derart hergestelltes bauteil und legeform |
US8771443B2 (en) * | 2012-01-05 | 2014-07-08 | The Boeing Company | Method of fabricating a composite laminate enabling structural monitoring using electromagnetic radiation |
FR2987778B1 (fr) * | 2012-03-12 | 2014-05-02 | Airbus Operations Sas | Procede de realisation d'un profile courbe en materiau composite a partir d'une preforme rectiligne de nappes de fibres |
FR2987779A1 (fr) * | 2012-03-12 | 2013-09-13 | Airbus Operations Sas | Procede de realisation d'une piece en materiau composite et outillage pour sa mise en oeuvre |
EP2899396B1 (fr) * | 2012-09-24 | 2017-08-16 | Mitsubishi Heavy Industries, Ltd. | Procédé de fabrication de pale d'éolienne |
US10137647B2 (en) | 2012-12-28 | 2018-11-27 | Compositence Gmbh | Method and device for manufacturing three-dimensional fiber fabrics and component preforms made of fibres in two steps |
US10583616B2 (en) * | 2014-06-20 | 2020-03-10 | The Boeing Company | Forming tools and flexible ultrasonic transducer arrays |
EP2985137B1 (fr) * | 2014-08-14 | 2017-10-11 | Airbus Operations GmbH | Procédé et appareil de formation d'éléments profilés |
CN104443426B (zh) * | 2014-10-08 | 2016-06-08 | 中国航空工业集团公司北京航空制造工程研究所 | 一种飞机钛合金框梁类零件制造方法 |
CN104527091B (zh) * | 2015-01-04 | 2017-05-31 | 中国科学院宁波材料技术与工程研究所 | 一种纤维布凸模的自动铺料装置 |
CN105984153A (zh) * | 2015-02-13 | 2016-10-05 | 全耐塑料公司 | 预成型预浸渍复合材料片时的铺设方法 |
CN105109059B (zh) * | 2015-09-14 | 2018-06-08 | 沈阳飞机工业(集团)有限公司 | 一种专用压辊的使用方法 |
DE102016002844B3 (de) * | 2016-03-10 | 2017-08-10 | Premium Aerotec Gmbh | Strukturbauteil, Verfahren zur Herstellung eines Strukturbauteils, Druckrumpf für ein Fahrzeug mit Strukturbauteil |
FR3061129B1 (fr) * | 2016-12-22 | 2019-05-31 | Airbus Operations | Procede de fabrication d'un module d'isolation thermophonique pour aeronef comprenant une etape de cintrage |
DE102017212860B4 (de) * | 2017-07-26 | 2020-07-09 | Premium Aerotec Gmbh | Vorrichtung und Verfahren zur Herstellung eines gekrümmten Faservorformlings aus einem bi- oder multidirektionalen Faserhalbzeug |
CN107187074B (zh) * | 2017-07-27 | 2019-03-22 | 北京汽车集团有限公司 | 减小复合材料u型制件变形的方法 |
FR3078010B1 (fr) * | 2018-02-16 | 2021-10-08 | Jerome Aubry | Materiau composite et procede de realisation de ce materiau |
JP6719495B2 (ja) * | 2018-03-06 | 2020-07-08 | 株式会社Subaru | プリフォーム賦形方法、複合材成形方法及び複合材 |
CN108357080B (zh) * | 2018-04-23 | 2023-05-23 | 常州新创航空科技有限公司 | 一种复合材料成型设备 |
DE102018212442A1 (de) * | 2018-07-25 | 2020-01-30 | Brose Fahrzeugteile Gmbh & Co. Kommanditgesellschaft, Coburg | Fahrzeugsitzgestell mit einem aus einem Faserverbundwerkstoff gefertigten Rohrelement |
JP7096106B2 (ja) | 2018-08-28 | 2022-07-05 | 株式会社Subaru | プリフォーム賦形方法及び複合材成形方法 |
JP7193282B2 (ja) * | 2018-09-14 | 2022-12-20 | 株式会社Subaru | プリフォーム賦形方法及び複合材成形方法 |
US11173675B2 (en) * | 2019-03-25 | 2021-11-16 | The Boeing Company | Automated fiber-placement systems and methods |
FR3100152B1 (fr) * | 2019-08-28 | 2021-07-23 | Safran Aircraft Engines | Procede de fabrication d’un carter annulaire pour une turbomachine d’aeronef |
CN111483156B (zh) * | 2020-04-08 | 2021-02-02 | 北京航天新风机械设备有限责任公司 | 一种复合材料大型薄壁含筋半罩铺层方法 |
Citations (6)
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GB1455572A (en) * | 1973-02-20 | 1976-11-17 | British Aircraft Corp Ltd | Beams of fibre reinforced plastics |
EP0606830A1 (fr) * | 1993-01-15 | 1994-07-20 | GFM Gesellschaft für Fertigungstechnik und Maschinenbau Aktiengesellschaft | Procédé de fabrication d'une plaque préimprégnée plastique renforcée de fibres |
EP1145829A1 (fr) * | 2000-04-14 | 2001-10-17 | Honda Giken Kogyo Kabushiki Kaisha | Procédé pour produire un produit intermédiaire fait d'un matériau composite renforcé par des fibres |
WO2005011961A1 (fr) * | 2003-08-01 | 2005-02-10 | Alliant Techsystems Inc. | Appareil et procedes de formation de raidisseurs composites et de structures de renforcement |
US20060243860A1 (en) * | 2005-04-28 | 2006-11-02 | The Boeing Company | Composite skin and stringer structure and method for forming the same |
US20070029038A1 (en) * | 2005-08-03 | 2007-02-08 | The Boeing Company | Composite structural element fabricating device and method |
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US5386217A (en) * | 1993-08-16 | 1995-01-31 | Winbond Electronic Corp. | Method for controlling a liquid crystal display module to show interlaced picture data thereon |
US5954917A (en) * | 1997-06-02 | 1999-09-21 | Boeing North American, Inc. | Automated material delivery system |
JP2001166280A (ja) * | 1999-12-10 | 2001-06-22 | Nec Corp | 液晶表示装置の駆動方法 |
NZ532360A (en) * | 2001-09-17 | 2005-12-23 | Verdant Technologies Inc | Three-dimensional knit spacer fabric sandwich composite |
JP2003241721A (ja) * | 2002-02-20 | 2003-08-29 | Fujitsu Display Technologies Corp | 液晶パネルの表示制御装置および液晶表示装置 |
JP2005031643A (ja) * | 2003-06-20 | 2005-02-03 | Sanyo Electric Co Ltd | 発光装置及び表示装置 |
GB0416197D0 (en) * | 2004-07-20 | 2004-08-18 | B I Group Plc | Composite plastic and related manufacturing methods |
US20080210372A1 (en) * | 2007-03-01 | 2008-09-04 | Cumings Robert C | Composite article debulking process |
-
2008
- 2008-03-07 FR FR0801261A patent/FR2928294B1/fr not_active Expired - Fee Related
-
2009
- 2009-03-05 EP EP09722505A patent/EP2262634A2/fr not_active Withdrawn
- 2009-03-05 US US12/920,922 patent/US20110086199A1/en not_active Abandoned
- 2009-03-05 CN CN200980113385.XA patent/CN102006986B/zh active Active
- 2009-03-05 WO PCT/FR2009/050357 patent/WO2009115734A2/fr active Application Filing
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1455572A (en) * | 1973-02-20 | 1976-11-17 | British Aircraft Corp Ltd | Beams of fibre reinforced plastics |
EP0606830A1 (fr) * | 1993-01-15 | 1994-07-20 | GFM Gesellschaft für Fertigungstechnik und Maschinenbau Aktiengesellschaft | Procédé de fabrication d'une plaque préimprégnée plastique renforcée de fibres |
EP1145829A1 (fr) * | 2000-04-14 | 2001-10-17 | Honda Giken Kogyo Kabushiki Kaisha | Procédé pour produire un produit intermédiaire fait d'un matériau composite renforcé par des fibres |
WO2005011961A1 (fr) * | 2003-08-01 | 2005-02-10 | Alliant Techsystems Inc. | Appareil et procedes de formation de raidisseurs composites et de structures de renforcement |
US20060243860A1 (en) * | 2005-04-28 | 2006-11-02 | The Boeing Company | Composite skin and stringer structure and method for forming the same |
US20070029038A1 (en) * | 2005-08-03 | 2007-02-08 | The Boeing Company | Composite structural element fabricating device and method |
Non-Patent Citations (1)
Title |
---|
DANIEL GAY: "Matériaux Composites", 1 January 1991, MATERIAUX COMPOSITES, XX, XX, PAGE(S) 107 - 111, XP002503806 * |
Also Published As
Publication number | Publication date |
---|---|
CN102006986B (zh) | 2014-01-08 |
FR2928294A1 (fr) | 2009-09-11 |
WO2009115734A2 (fr) | 2009-09-24 |
FR2928294B1 (fr) | 2016-12-30 |
US20110086199A1 (en) | 2011-04-14 |
EP2262634A2 (fr) | 2010-12-22 |
CN102006986A (zh) | 2011-04-06 |
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