DE602005010105D1 - Verfahren zur Herstellung eines integralen Formteils aus faserverstärktem Verbundwerkstoff und Werkzeugsystem zur Herstellung desselben - Google Patents

Verfahren zur Herstellung eines integralen Formteils aus faserverstärktem Verbundwerkstoff und Werkzeugsystem zur Herstellung desselben

Info

Publication number
DE602005010105D1
DE602005010105D1 DE602005010105T DE602005010105T DE602005010105D1 DE 602005010105 D1 DE602005010105 D1 DE 602005010105D1 DE 602005010105 T DE602005010105 T DE 602005010105T DE 602005010105 T DE602005010105 T DE 602005010105T DE 602005010105 D1 DE602005010105 D1 DE 602005010105D1
Authority
DE
Germany
Prior art keywords
composite material
producing
fiber
reinforced composite
same
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
DE602005010105T
Other languages
English (en)
Inventor
Peter Greis
Max Krogager
Mikael Petersson
Bjoern Weidmann
Torbjoern Alenby
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.)
Saab AB
Original Assignee
Saab AB
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 Saab AB filed Critical Saab AB
Publication of DE602005010105D1 publication Critical patent/DE602005010105D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B29C33/52—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 soluble or fusible
    • 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
    • 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
    • B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/17—Component parts, details or accessories; Auxiliary operations
    • B29C45/72—Heating or cooling
    • B29C45/73—Heating or cooling of the mould
    • B29C2045/7393—Heating or cooling of the mould alternately heating and cooling
DE602005010105T 2005-12-20 2005-12-20 Verfahren zur Herstellung eines integralen Formteils aus faserverstärktem Verbundwerkstoff und Werkzeugsystem zur Herstellung desselben Active DE602005010105D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP05112451A EP1800825B1 (de) 2005-12-20 2005-12-20 Verfahren zur Herstellung eines integralen Formteils aus faserverstärktem Verbundwerkstoff und Werkzeugsystem zur Herstellung desselben

Publications (1)

Publication Number Publication Date
DE602005010105D1 true DE602005010105D1 (de) 2008-11-13

Family

ID=35929989

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005010105T Active DE602005010105D1 (de) 2005-12-20 2005-12-20 Verfahren zur Herstellung eines integralen Formteils aus faserverstärktem Verbundwerkstoff und Werkzeugsystem zur Herstellung desselben

Country Status (5)

Country Link
US (1) US20070221322A1 (de)
EP (1) EP1800825B1 (de)
AT (1) ATE409567T1 (de)
DE (1) DE602005010105D1 (de)
ES (1) ES2313230T3 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2937278B1 (fr) * 2008-10-22 2013-02-08 Eads Europ Aeronautic Defence Procede de realisation de pieces de formes creuses en materiau composite
DE102008044069B3 (de) 2008-11-26 2010-08-05 Airbus Deutschland Gmbh Formkörper zur Herstellung eines Faserverbundbauteils
GB2470618B (en) * 2009-09-14 2011-08-24 Alexander Fergusson An improved method of and apparatus for making a composite material
US9145203B2 (en) 2012-10-31 2015-09-29 The Boeing Company Natural laminar flow wingtip
US9498903B2 (en) 2012-10-31 2016-11-22 The Boeing Company System and method for manufacturing monolithic structures using expanding internal tools
US9199419B2 (en) 2012-10-31 2015-12-01 The Boeing Company System and method for facilitating fluid movement in close-molded composite parts
US9481136B2 (en) 2012-10-31 2016-11-01 The Boeing Company Over-molded vacuum barrier and inner mold line bag carrier with soluble details in trapped closed mold tooling
CN103600500B (zh) * 2013-10-31 2016-04-06 徐建昇 中空纤维管制作方法
JP6209095B2 (ja) * 2014-01-31 2017-10-04 三菱重工業株式会社 Ｆｒｐ成形治具及びｆｒｐ構造体の成形方法
US11034431B2 (en) 2017-09-25 2021-06-15 The Boeing Company Composite article with fly-away bag carrier
KR102188243B1 (ko) 2018-08-08 2020-12-08 전북대학교산학협력단 Vartm을 이용한 복합재료의 성형 장치 및 방법
CN113103615B (zh) * 2021-03-19 2022-08-12 航天材料及工艺研究所 一种复合材料低温贮箱的整体成型工艺方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS57181819A (en) * 1981-05-02 1982-11-09 Toyota Motor Corp Forming method of resin mold having undercut shape
JPS6169436A (ja) 1984-09-11 1986-04-10 Hitachi Zosen Corp 発泡型材を使用した物品成型法
US4853172A (en) * 1987-12-01 1989-08-01 United Technologies Corporation Method of fabricating tubular composite structures
JPH0490330A (ja) * 1990-08-06 1992-03-24 Mitsubishi Plastics Ind Ltd 繊維強化プラスチックファンの製法
FR2760399B1 (fr) * 1997-03-06 1999-05-07 Hispano Suiza Sa Procede de fabrication de pieces creuses en materiau composite
US6921503B1 (en) * 2002-12-02 2005-07-26 Foam Matrix, Inc. Lost foam molding

Also Published As

Publication number Publication date
EP1800825A1 (de) 2007-06-27
US20070221322A1 (en) 2007-09-27
EP1800825B1 (de) 2008-10-01
ES2313230T3 (es) 2009-03-01
ATE409567T1 (de) 2008-10-15

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