CA2188629A1 - Process for the production of a composite material panel with resin transfer moulding - Google Patents
Process for the production of a composite material panel with resin transfer mouldingInfo
- Publication number
- CA2188629A1 CA2188629A1 CA002188629A CA2188629A CA2188629A1 CA 2188629 A1 CA2188629 A1 CA 2188629A1 CA 002188629 A CA002188629 A CA 002188629A CA 2188629 A CA2188629 A CA 2188629A CA 2188629 A1 CA2188629 A1 CA 2188629A1
- Authority
- CA
- Canada
- Prior art keywords
- fibres
- production
- composite material
- mould
- core
- 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
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
- 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
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
-
- 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
-
- 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
- B29L2024/00—Articles with hollow walls
-
- 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
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
For the production of a composite material sandwich panel having an open cell core (18) and at least one skin formed from resin impregnated fibres (20), the core (18) and unimpregnated fibres (20) are placed in a mould (10) and a tight membrane (22) and an adhesive film (24) are interposed in this order between the fibres and the core. After closing the mould (10), a single heat cycle makes it possible to polymerize the adhesive (20), in order to seal the cavities of the open cell core (18) with the membrane, followed by the injection of the resin under pressure into the fibres (20) and finally polymerize said resin prior to the removal of the panel from the mould.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9512727 | 1995-10-27 | ||
FR9512727A FR2740383B1 (en) | 1995-10-27 | 1995-10-27 | METHOD FOR MANUFACTURING A COMPOSITE MATERIAL PANEL WITH RESIN TRANSFER MOLDING |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2188629A1 true CA2188629A1 (en) | 1997-04-28 |
CA2188629C CA2188629C (en) | 2005-06-21 |
Family
ID=9484007
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA002188629A Expired - Fee Related CA2188629C (en) | 1995-10-27 | 1996-10-23 | Process for the production of a composite material panel with resin transfer moulding |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP0770472B1 (en) |
AU (1) | AU709483B2 (en) |
CA (1) | CA2188629C (en) |
DE (1) | DE69605884T2 (en) |
ES (1) | ES2143161T3 (en) |
FR (1) | FR2740383B1 (en) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2195050A1 (en) * | 1996-01-29 | 1997-07-30 | Mark David Thiede-Smet | Low-weight and water-resistant honeycomb sandwich panels made by resin transfer molding process |
FR2764525B1 (en) | 1997-06-13 | 1999-07-23 | Commissariat Energie Atomique | ATTACHMENT OR SEPARATION OF IONS, PARTICULARLY PB, BY DERIVATIVES OF PER (3.6 ANHYDRO) CYCLODEXTRINS |
JP4342620B2 (en) * | 1998-12-02 | 2009-10-14 | 富士重工業株式会社 | Method for forming honeycomb sandwich structure composite panel |
FR2798618B1 (en) | 1999-09-21 | 2002-05-03 | Aerospatiale Matra Airbus | METHOD FOR MANUFACTURING A SANDWICH PANEL MADE OF COMPOSITE MATERIAL, AND A PANEL THUS OBTAINED |
DE10007373C1 (en) * | 2000-02-18 | 2000-11-23 | Daimler Chrysler Aerospace | Sandwich component manufacture for aerospace products involves injecting resin mixture onto core covered with dry reinforcement, gelling and then finally closing tool |
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 |
US7226559B2 (en) * | 2000-12-08 | 2007-06-05 | Toyota Motor Sales, U.S.A., Inc. | Method for molding structures |
US7124797B2 (en) | 2001-03-02 | 2006-10-24 | Toyota Motor Sales, Usa, Inc. | Filament winding apparatus and methods of winding filament |
DE10146201B4 (en) * | 2001-09-13 | 2005-10-27 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Method for producing a fiber composite part and component made of a fiber composite material |
DE60220620T2 (en) * | 2001-10-30 | 2008-02-14 | The Boeing Co., Chicago | Woodcore core composite articles and methods of making the same |
GB0213161D0 (en) * | 2002-06-07 | 2002-07-17 | Short Brothers Plc | A fibre reinforced composite component |
US7559332B2 (en) | 2002-07-02 | 2009-07-14 | Toyota Motor Sales U.S.A., Inc. | Media removal apparatus and methods of removing media |
US7101452B2 (en) | 2002-07-19 | 2006-09-05 | Toyota Motor Sales Usa, Inc. | Methods of debonding a composite tooling |
US7217380B2 (en) | 2002-07-22 | 2007-05-15 | Toyota Motor Sales, Usa, Inc. | Vibration apparatus and methods of vibration |
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 |
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 |
EP1972550B1 (en) * | 2007-03-19 | 2015-04-29 | Liebherr-Aerospace Lindenberg GmbH | Airplane landing gear |
DE102007021277B4 (en) * | 2007-05-07 | 2009-08-13 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Process for producing a support structure and a support structure |
DE102009017512A1 (en) | 2009-04-15 | 2010-10-28 | Airbus Deutschland Gmbh | Producing a composite component |
JP5686994B2 (en) * | 2010-07-01 | 2015-03-18 | 三菱重工業株式会社 | Manufacturing method of molded body |
FR2970899B1 (en) * | 2011-01-28 | 2014-08-22 | Aircelle Sa | PROCESS FOR MANUFACTURING A ROOM OF TURBOREACTOR NACELLE |
WO2013050074A1 (en) | 2011-10-05 | 2013-04-11 | Basf Se | Method for producing fiber-reinforced composite materials |
FR2989310B1 (en) * | 2012-04-11 | 2014-04-04 | Aircelle Sa | METHOD FOR MANUFACTURING SANDWICH PANEL COMPOSITE WITH ALVEOLAR SOUL |
DE102013012005B4 (en) * | 2013-07-18 | 2022-05-05 | Technische Universität München | Process for manufacturing a component from a fiber composite material |
FR3089854B1 (en) | 2018-12-18 | 2022-02-04 | Saint Gobain Performance Plastics France | METHOD FOR PREPARING A COMPOSITE MATERIAL IN THE FORM OF A SANDWICH |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2440261A1 (en) * | 1978-10-31 | 1980-05-30 | Krieg & Zivy Ind | Moulding door panels with reinforced resin covers - to obtain durable composite structures with good dimensional stability |
US4891176A (en) * | 1988-05-31 | 1990-01-02 | Auto-Fab, Inc. | Resin transfer molding process |
US4954382A (en) * | 1988-11-01 | 1990-09-04 | American Cyanamid Company | Interleaf layer in fiber reinforced resin laminate composites |
US5141804A (en) | 1988-11-01 | 1992-08-25 | American Cyanamid Company | Interleaf layer in fiber reinforced resin laminate composites |
GB8915369D0 (en) * | 1989-07-04 | 1989-08-23 | 3 D Composites | Moulding method |
EP0441249A1 (en) * | 1990-02-05 | 1991-08-14 | Takeda Chemical Industries, Ltd. | A racket frame and production thereof |
US5567499A (en) * | 1995-01-03 | 1996-10-22 | The Boeing Company | Resin transfer molding in combination with honeycomb core |
-
1995
- 1995-10-27 FR FR9512727A patent/FR2740383B1/en not_active Expired - Fee Related
-
1996
- 1996-10-22 AU AU70335/96A patent/AU709483B2/en not_active Ceased
- 1996-10-23 CA CA002188629A patent/CA2188629C/en not_active Expired - Fee Related
- 1996-10-24 EP EP96402266A patent/EP0770472B1/en not_active Expired - Lifetime
- 1996-10-24 ES ES96402266T patent/ES2143161T3/en not_active Expired - Lifetime
- 1996-10-24 DE DE69605884T patent/DE69605884T2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0770472A1 (en) | 1997-05-02 |
ES2143161T3 (en) | 2000-05-01 |
CA2188629C (en) | 2005-06-21 |
FR2740383B1 (en) | 1998-01-16 |
AU7033596A (en) | 1997-05-01 |
AU709483B2 (en) | 1999-08-26 |
FR2740383A1 (en) | 1997-04-30 |
EP0770472B1 (en) | 1999-12-29 |
DE69605884T2 (en) | 2000-07-20 |
DE69605884D1 (en) | 2000-02-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |