DE69605884T2 - Verfahren zur Herstellung einer Platte aus Verbundmaterial durch Transfer-Giessverfahren - Google Patents

Verfahren zur Herstellung einer Platte aus Verbundmaterial durch Transfer-Giessverfahren

Info

Publication number
DE69605884T2
DE69605884T2 DE69605884T DE69605884T DE69605884T2 DE 69605884 T2 DE69605884 T2 DE 69605884T2 DE 69605884 T DE69605884 T DE 69605884T DE 69605884 T DE69605884 T DE 69605884T DE 69605884 T2 DE69605884 T2 DE 69605884T2
Authority
DE
Germany
Prior art keywords
sheet
producing
composite material
transfer molding
molding
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.)
Expired - Lifetime
Application number
DE69605884T
Other languages
English (en)
Other versions
DE69605884D1 (de
Inventor
Dominique Guittard
Daniel Soro
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Publication of DE69605884D1 publication Critical patent/DE69605884D1/de
Application granted granted Critical
Publication of DE69605884T2 publication Critical patent/DE69605884T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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)
DE69605884T 1995-10-27 1996-10-24 Verfahren zur Herstellung einer Platte aus Verbundmaterial durch Transfer-Giessverfahren Expired - Lifetime DE69605884T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9512727A FR2740383B1 (fr) 1995-10-27 1995-10-27 Procede de fabrication d'un panneau en materiau composite avec moulage par transfert de resine

Publications (2)

Publication Number Publication Date
DE69605884D1 DE69605884D1 (de) 2000-02-03
DE69605884T2 true DE69605884T2 (de) 2000-07-20

Family

ID=9484007

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69605884T Expired - Lifetime DE69605884T2 (de) 1995-10-27 1996-10-24 Verfahren zur Herstellung einer Platte aus Verbundmaterial durch Transfer-Giessverfahren

Country Status (6)

Country Link
EP (1) EP0770472B1 (de)
AU (1) AU709483B2 (de)
CA (1) CA2188629C (de)
DE (1) DE69605884T2 (de)
ES (1) ES2143161T3 (de)
FR (1) FR2740383B1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10146201A1 (de) * 2001-09-13 2003-04-10 Deutsch Zentr Luft & Raumfahrt Verfahren zur Herstellung eines Faserverbundwerkstoffteils und Bauteil aus einem Faserverbundwerkstoff
DE102013012005A1 (de) * 2013-07-18 2015-01-22 Technische Universität München Verfahren zur Herstellung eines Bauteils aus einem Faserverbundwerkstoff

Families Citing this family (23)

* Cited by examiner, † Cited by third party
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 (fr) 1997-06-13 1999-07-23 Commissariat Energie Atomique Fixation ou separation d'ions, notamment de pb, par des derives de per (3,6 anhydro) cyclodextrines
JP4342620B2 (ja) * 1998-12-02 2009-10-14 富士重工業株式会社 ハニカムサンドイッチ構造複合材パネルの成形方法
FR2798618B1 (fr) 1999-09-21 2002-05-03 Aerospatiale Matra Airbus Procede de fabrication d'un panneau sandwich en materiau composite, et panneau ainsi obtenu
DE10007373C1 (de) * 2000-02-18 2000-11-23 Daimler Chrysler Aerospace Verfahren zur Herstellung von Sandwichbauteilen
US6823578B2 (en) 2000-11-15 2004-11-30 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
DE60220620T2 (de) * 2001-10-30 2008-02-14 The Boeing Co., Chicago Holzzellenkern-Verbundwerkstoffgegenstände und Verfahren zu deren Herstellung
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 (de) * 2007-03-19 2015-04-29 Liebherr-Aerospace Lindenberg GmbH Flugzeugfahrwerk
DE102007021277B4 (de) * 2007-05-07 2009-08-13 Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. Verfahren zur Herstellung einer Stützstruktur sowie eine Stützstruktur
DE102009017512A1 (de) 2009-04-15 2010-10-28 Airbus Deutschland Gmbh Herstellen eines Verbundbauteils
JP5686994B2 (ja) * 2010-07-01 2015-03-18 三菱重工業株式会社 成形体の製造方法
FR2970899B1 (fr) * 2011-01-28 2014-08-22 Aircelle Sa Procede de fabrication d'une piece de nacelle de turboreacteur
CN103826833A (zh) 2011-10-05 2014-05-28 巴斯夫欧洲公司 制备纤维增强的复合材料的方法
FR2989310B1 (fr) * 2012-04-11 2014-04-04 Aircelle Sa Procede de fabrication d'un panneau sandwich composite a ame alveolaire
FR3089854B1 (fr) 2018-12-18 2022-02-04 Saint Gobain Performance Plastics France Procede de preparation d’un materiau composite sous forme de sandwich

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2440261A1 (fr) * 1978-10-31 1980-05-30 Krieg & Zivy Ind Procede et moule pour la realisation d'un quelconque produit a parement en matiere synthetique, et produit correspondant
US4891176A (en) * 1988-05-31 1990-01-02 Auto-Fab, Inc. Resin transfer molding process
US5141804A (en) 1988-11-01 1992-08-25 American Cyanamid Company Interleaf layer in fiber reinforced resin laminate composites
US4954382A (en) * 1988-11-01 1990-09-04 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 (de) * 1990-02-05 1991-08-14 Takeda Chemical Industries, Ltd. Schlägerrahmen und dessen Herstellung
US5567499A (en) * 1995-01-03 1996-10-22 The Boeing Company Resin transfer molding in combination with honeycomb core

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10146201A1 (de) * 2001-09-13 2003-04-10 Deutsch Zentr Luft & Raumfahrt Verfahren zur Herstellung eines Faserverbundwerkstoffteils und Bauteil aus einem Faserverbundwerkstoff
DE10146201B4 (de) * 2001-09-13 2005-10-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur Herstellung eines Faserverbundwerkstoffteils und Bauteil aus einem Faserverbundwerkstoff
DE102013012005A1 (de) * 2013-07-18 2015-01-22 Technische Universität München Verfahren zur Herstellung eines Bauteils aus einem Faserverbundwerkstoff
DE102013012005B4 (de) 2013-07-18 2022-05-05 Technische Universität München Verfahren zur Herstellung eines Bauteils aus einem Faserverbundwerkstoff

Also Published As

Publication number Publication date
FR2740383A1 (fr) 1997-04-30
CA2188629C (en) 2005-06-21
AU7033596A (en) 1997-05-01
EP0770472B1 (de) 1999-12-29
AU709483B2 (en) 1999-08-26
DE69605884D1 (de) 2000-02-03
ES2143161T3 (es) 2000-05-01
CA2188629A1 (en) 1997-04-28
EP0770472A1 (de) 1997-05-02
FR2740383B1 (fr) 1998-01-16

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