SE519225C2 - Metod för framställning av konstruktionsdelar av fiberförstärkt plast med icke fullständigt utvikningsbar geometri - Google Patents

Metod för framställning av konstruktionsdelar av fiberförstärkt plast med icke fullständigt utvikningsbar geometri

Info

Publication number
SE519225C2
SE519225C2 SE0001065A SE0001065A SE519225C2 SE 519225 C2 SE519225 C2 SE 519225C2 SE 0001065 A SE0001065 A SE 0001065A SE 0001065 A SE0001065 A SE 0001065A SE 519225 C2 SE519225 C2 SE 519225C2
Authority
SE
Sweden
Prior art keywords
finished product
semi
textile
textile semi
curing device
Prior art date
Application number
SE0001065A
Other languages
English (en)
Swedish (sv)
Other versions
SE0001065D0 (sv
SE0001065L (sv
Inventor
Olaf Rocker
Franz Stadler
Stefan Utecht
Original Assignee
Daimler Chrysler Ag
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 Daimler Chrysler Ag filed Critical Daimler Chrysler Ag
Publication of SE0001065D0 publication Critical patent/SE0001065D0/xx
Publication of SE0001065L publication Critical patent/SE0001065L/
Publication of SE519225C2 publication Critical patent/SE519225C2/sv

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
    • B29C70/30—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
    • 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)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Reinforced Plastic Materials (AREA)
SE0001065A 1999-04-01 2000-03-24 Metod för framställning av konstruktionsdelar av fiberförstärkt plast med icke fullständigt utvikningsbar geometri SE519225C2 (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19915083A DE19915083C1 (de) 1999-04-01 1999-04-01 Verfahren zur Herstellung faserverstärkter Kunststoffbauteile mit nicht-vollständig abwickelbarer Geometrie

Publications (3)

Publication Number Publication Date
SE0001065D0 SE0001065D0 (sv) 2000-03-24
SE0001065L SE0001065L (sv) 2000-10-02
SE519225C2 true SE519225C2 (sv) 2003-02-04

Family

ID=7903389

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0001065A SE519225C2 (sv) 1999-04-01 2000-03-24 Metod för framställning av konstruktionsdelar av fiberförstärkt plast med icke fullständigt utvikningsbar geometri

Country Status (6)

Country Link
US (1) US6527894B1 (fr)
DE (1) DE19915083C1 (fr)
ES (1) ES2176076B2 (fr)
FR (1) FR2791600B1 (fr)
GB (1) GB2351937B (fr)
SE (1) SE519225C2 (fr)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19915083C1 (de) 1999-04-01 2000-04-13 Daimler Chrysler Ag Verfahren zur Herstellung faserverstärkter Kunststoffbauteile mit nicht-vollständig abwickelbarer Geometrie
DE10062899A1 (de) * 2000-12-16 2002-06-20 Volkswagen Ag Verfahren und Vorrichtung zur Herstellung eines Innenverkleidungsteils eines Fahrzeugs, insbesondere eines Kraftfahrzeugs, sowie Innenverkleidungsteil
DE10156123B4 (de) * 2001-11-16 2006-07-27 Eads Deutschland Gmbh Verfahren und Vorrichtung zur Herstellung von faserverstärkten Kunststoffbauteilen
US7052573B2 (en) * 2003-11-21 2006-05-30 The Boeing Company Method to eliminate undulations in a composite panel
US7332049B2 (en) * 2004-12-22 2008-02-19 General Electric Company Method for fabricating reinforced composite materials
DE102006002198B4 (de) * 2006-01-16 2011-04-28 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbund-Bauelements
EP1851036B1 (fr) 2005-02-21 2012-10-03 Airbus Operations GmbH Element composite renforce par des fibres et procede de production d'un element composite renforce par des fibres
DE102005008252B4 (de) * 2005-02-21 2014-03-20 Airbus Operations Gmbh Verfahren zur Herstellung eines Faserverbund-Bauelements
DE102005026010B4 (de) * 2005-06-07 2010-12-30 Airbus Deutschland Gmbh Verfahren zur Herstellung einer verstärkten Schale zur Bildung von Teilkomponenten für Luftfahrzeuge
US7633040B2 (en) * 2005-11-14 2009-12-15 The Boeing Company Bulk resin infusion system apparatus and method
GB2447964B (en) * 2007-03-29 2012-07-18 Gurit Uk Ltd Moulding material
US8449709B2 (en) 2007-05-25 2013-05-28 The Boeing Company Method of fabricating fiber reinforced composite structure having stepped surface
DE102007048449A1 (de) 2007-10-10 2009-04-23 Eads Deutschland Gmbh Auftriebsklappenträgersystem
ITTO20070796A1 (it) * 2007-11-08 2009-05-09 Alenia Aeronautica Spa Attrezzatura per infusione di resina in una preforma in stampo chiuso.
DE102008015070B3 (de) * 2008-03-19 2009-10-01 Eurocopter Deutschland Gmbh VAP-Autoklav-Verfahren zur Herstellung von Faserverbundbauteilen und Vorrichtung dafür
DE102009047340B4 (de) * 2009-12-01 2011-07-14 Airbus Operations GmbH, 21129 Verfahren zum Bilden eines Strukturbauteils eines Luft- oder Raumfahrzeuges und Umformvorrichtung
CN103097116B (zh) 2010-07-02 2016-11-09 赫克赛尔控股有限责任公司 纤维增强复合材料模制品
DE102011006032A1 (de) * 2011-03-24 2012-09-27 Airbus Operations Gmbh Verfahren zur Herstellung eines Strukturbauteils sowie Strukturbauteil
DE102011079947A1 (de) * 2011-07-27 2013-01-31 Airbus Operations Gmbh Vorrichtung zur Herstellung eines Klebebauteils mit Faserverbundkunststoffen sowie Verfahren
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
US20140166191A1 (en) * 2012-12-14 2014-06-19 Aurora Flight Sciences Corporation Methods for combining components of varying stages of cure
CN103963319B (zh) * 2014-05-29 2016-06-15 上海飞机制造有限公司 一种复合材料加筋壁板的预浸料/树脂膜熔渗共固化成型方法
CN105904828A (zh) * 2016-05-04 2016-08-31 哈尔滨飞机工业集团有限责任公司 一种飞机上板-板零件的成型方法
DE102016116024B4 (de) 2016-08-29 2021-05-12 Deutsches Zentrum für Luft- und Raumfahrt e.V. Herstellen eines Faserverbundformteils durch sequenzielle Infusion
US11332228B2 (en) 2018-04-06 2022-05-17 Aurora Flight Sciences Corporation Aircraft fuselage with composite pre-form

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JPS59165647A (ja) * 1983-03-10 1984-09-18 東レ株式会社 複合材料用補強材
US4622091A (en) * 1984-11-29 1986-11-11 The Boeing Company Resin film infusion process and apparatus
US4816106A (en) * 1984-12-13 1989-03-28 Aeritalia Saipa - Gruppo Velivoli Da Trasporto Method for the controlled curing of composites
US4786343A (en) * 1985-05-10 1988-11-22 The Boeing Company Method of making delamination resistant composites
US4942013A (en) * 1989-03-27 1990-07-17 Mcdonnell Douglas Corporation Vacuum resin impregnation process
JPH03109437A (ja) * 1989-09-21 1991-05-09 Sekisui Chem Co Ltd 光硬化性プリプレグシート及びその複合成形体の製造方法
JPH03109436A (ja) * 1989-09-21 1991-05-09 Sekisui Chem Co Ltd 光硬化性プリプレグシート及び複合成形体の製造方法
US5593633A (en) * 1990-05-03 1997-01-14 Dull; Kenneth M. Edge and surface breather for high temperature composite processing
US5281388A (en) * 1992-03-20 1994-01-25 Mcdonnell Douglas Corporation Resin impregnation process for producing a resin-fiber composite
US5433165A (en) 1994-03-30 1995-07-18 Outboard Marine Corporation Method of manufacturing a boat hull
JPH07276233A (ja) * 1994-04-08 1995-10-24 Mitsubishi Heavy Ind Ltd 複合材製多孔面板の製造方法
US5567499A (en) * 1995-01-03 1996-10-22 The Boeing Company Resin transfer molding in combination with honeycomb core
FR2744054B1 (fr) * 1996-01-29 1998-04-30 Aerospatiale Procede de realisation de pieces en materiau composite a haute precision dimensionnelle mettant en oeuvre une polymerisation par ionisation et pieces ainsi obtenues
US5980665A (en) * 1996-05-31 1999-11-09 The Boeing Company Z-pin reinforced bonds for connecting composite structures
US6139942A (en) * 1997-02-06 2000-10-31 Cytec Technology, Inc. Resin composition, a fiber reinforced material having a partially impregnated resin and composites made therefrom
DE19813104A1 (de) * 1998-03-25 1999-09-30 Daimler Chrysler Ag Verfahren zur Herstellung von Faserverbundbauteilen
DE19915083C1 (de) * 1999-04-01 2000-04-13 Daimler Chrysler Ag Verfahren zur Herstellung faserverstärkter Kunststoffbauteile mit nicht-vollständig abwickelbarer Geometrie

Also Published As

Publication number Publication date
FR2791600B1 (fr) 2005-02-25
GB0007914D0 (en) 2000-05-17
ES2176076A1 (es) 2002-11-16
GB2351937A (en) 2001-01-17
US6527894B1 (en) 2003-03-04
FR2791600A1 (fr) 2000-10-06
DE19915083C1 (de) 2000-04-13
SE0001065D0 (sv) 2000-03-24
GB2351937B (en) 2004-01-07
SE0001065L (sv) 2000-10-02
ES2176076B2 (es) 2003-08-01

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