DE602005027434D1 - Verfahren zur Herstellung faserverstärkter Verbundwerkstoffen - Google Patents

Verfahren zur Herstellung faserverstärkter Verbundwerkstoffen

Info

Publication number
DE602005027434D1
DE602005027434D1 DE200560027434 DE602005027434T DE602005027434D1 DE 602005027434 D1 DE602005027434 D1 DE 602005027434D1 DE 200560027434 DE200560027434 DE 200560027434 DE 602005027434 T DE602005027434 T DE 602005027434T DE 602005027434 D1 DE602005027434 D1 DE 602005027434D1
Authority
DE
Germany
Prior art keywords
composite materials
reinforced composite
producing fiber
fiber
producing
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
Application number
DE200560027434
Other languages
English (en)
Inventor
Masashi Ishii
Peter Mitschang
Florian Weyrauch
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.)
Honda Motor Co Ltd
Original Assignee
Honda Motor Co Ltd
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 Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Publication of DE602005027434D1 publication Critical patent/DE602005027434D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping 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
    • B29C70/48Shaping 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543Fixing the position or configuration of fibrous reinforcements before or during moulding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/54Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/546Measures for feeding or distributing the matrix material in the reinforcing structure
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/249921Web or sheet containing structurally defined element or component
    • Y10T428/249924Noninterengaged fiber-containing paper-free web or sheet which is not of specified porosity
DE200560027434 2005-02-01 2005-02-01 Verfahren zur Herstellung faserverstärkter Verbundwerkstoffen Active DE602005027434D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP20050002047 EP1685947B1 (de) 2005-02-01 2005-02-01 Verfahren zur Herstellung faserverstärkter Verbundwerkstoffen

Publications (1)

Publication Number Publication Date
DE602005027434D1 true DE602005027434D1 (de) 2011-05-26

Family

ID=34933544

Family Applications (1)

Application Number Title Priority Date Filing Date
DE200560027434 Active DE602005027434D1 (de) 2005-02-01 2005-02-01 Verfahren zur Herstellung faserverstärkter Verbundwerkstoffen

Country Status (4)

Country Link
US (1) US20060216490A1 (de)
EP (1) EP1685947B1 (de)
JP (1) JP2006213059A (de)
DE (1) DE602005027434D1 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8632653B2 (en) 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
DE102007060739B4 (de) 2007-12-17 2011-11-10 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Vorrichtung zur Herstellung von Faserverbundbauteilen
FR2926242B1 (fr) * 2008-01-16 2010-03-19 Eads Europ Aeronautic Defence Procede et dispositif de moulage d'une piece en composite thermoplastique a hautes performances
FR2926241B1 (fr) * 2008-01-16 2013-03-15 Eads Europ Aeronautic Defence Procede et dispositif de moulage d'une piece en materiau composite
US9090028B2 (en) 2008-04-17 2015-07-28 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US8349105B2 (en) 2008-04-17 2013-01-08 The Boeing Company Curved composite frames and method of making the same
US8932423B2 (en) * 2008-04-17 2015-01-13 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US9278484B2 (en) 2008-04-17 2016-03-08 The Boeing Company Method and apparatus for producing contoured composite structures and structures produced thereby
DE102009053549A1 (de) 2009-11-18 2011-05-19 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur Herstellung eines Faserverbundbauteils
US9475468B2 (en) * 2011-05-09 2016-10-25 Petroceramics S.P.A. Caliper bodies made from thermoplastic material
US20190226538A1 (en) * 2016-08-31 2019-07-25 Meggitt Aircraft Braking Systems Corporation Long-strand carbon composite brake housing
JP6831662B2 (ja) 2016-09-12 2021-02-17 川崎重工業株式会社 繊維強化プラスチック成形体の製造方法
US10501595B2 (en) * 2016-10-25 2019-12-10 The Boeing Company Insertion of catalyst into dry carbon fibers prior to resin impregnation
DE102016221510A1 (de) * 2016-11-03 2018-05-03 Bayerische Motoren Werke Aktiengesellschaft Partielle Faserhalbzeugfixierung und Faserverwerfungsaufnahme im RTM-Prozess
DE102018203722A1 (de) * 2018-03-13 2019-09-19 Bayerische Motoren Werke Aktiengesellschaft Verfahren zur Herstellung eines Faserverbundbauteils
JPWO2022185387A1 (de) * 2021-03-01 2022-09-09

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3780928T2 (de) * 1986-12-19 1992-12-24 Takeda Chemical Industries Ltd Verfahren zum gussformen von faserverstaerkten kunststoffen.
US5187001A (en) * 1990-09-26 1993-02-16 Gencorp Inc. Resin transfer molding apparatus
US5279892A (en) * 1992-06-26 1994-01-18 General Electric Company Composite airfoil with woven insert
US6250193B1 (en) * 1996-12-02 2001-06-26 A & P Technology, Inc. Braided structure with elastic bias strands
JP3991439B2 (ja) 1997-08-04 2007-10-17 東レ株式会社 繊維強化プラスチックおよび繊維強化プラスチックの成形方法
FR2783197B1 (fr) * 1998-09-15 2000-12-01 Peugeot Procede et dispositif de fabrication par moulage d'une piece comportant au moins une couche de renfort en fibres de verre
DE29904191U1 (de) * 1999-03-09 1999-05-27 Pott Richard Kettfaden-Faserschicht
DE60011503T2 (de) * 1999-04-13 2004-11-04 Fanuc Ltd. Verfahren, Vorrichtung und Medium zur Erstellung von Giessformbedingungen, und Giessformmaschine
JP2003020542A (ja) 2001-07-06 2003-01-24 Toray Ind Inc 炭素繊維布帛、成形方法、炭素繊維強化プラスチックおよび航空機構造部材

Also Published As

Publication number Publication date
EP1685947B1 (de) 2011-04-13
US20060216490A1 (en) 2006-09-28
JP2006213059A (ja) 2006-08-17
EP1685947A1 (de) 2006-08-02

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