DE602005005714D1 - Kontinuierliches pultrusionsverfahren zur herstellung von hochleistungs-strukturprofilen - Google Patents

Kontinuierliches pultrusionsverfahren zur herstellung von hochleistungs-strukturprofilen

Info

Publication number
DE602005005714D1
DE602005005714D1 DE200560005714 DE602005005714T DE602005005714D1 DE 602005005714 D1 DE602005005714 D1 DE 602005005714D1 DE 200560005714 DE200560005714 DE 200560005714 DE 602005005714 T DE602005005714 T DE 602005005714T DE 602005005714 D1 DE602005005714 D1 DE 602005005714D1
Authority
DE
Germany
Prior art keywords
pultrusion process
impregnated
production
structural profiles
resin composition
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
DE200560005714
Other languages
English (en)
Other versions
DE602005005714T2 (de
Inventor
Roman Hillermeier
Lars Friedrich
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 Operations GmbH
Original Assignee
Hexcel Composites GmbH
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 Hexcel Composites GmbH filed Critical Hexcel Composites GmbH
Publication of DE602005005714D1 publication Critical patent/DE602005005714D1/de
Application granted granted Critical
Publication of DE602005005714T2 publication Critical patent/DE602005005714T2/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
    • 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
    • B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
    • B29C70/52—Pultrusion, i.e. forming and compressing by continuously pulling through a die
    • B29C70/525—Component parts, details or accessories; Auxiliary operations
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/40—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the curing agents used
    • C08G59/50—Amines
    • C—CHEMISTRY; METALLURGY
    • C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
    • C08G—MACROMOLECULAR COMPOUNDS OBTAINED OTHERWISE THAN BY REACTIONS ONLY INVOLVING UNSATURATED CARBON-TO-CARBON BONDS
    • C08G59/00—Polycondensates containing more than one epoxy group per molecule; Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups
    • C08G59/18—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing
    • C08G59/40—Macromolecules obtained by polymerising compounds containing more than one epoxy group per molecule using curing agents or catalysts which react with the epoxy groups ; e.g. general methods of curing characterised by the curing agents used
    • C08G59/50—Amines
    • C08G59/5033—Amines aromatic
    • D—TEXTILES; PAPER
    • D06—TREATMENT OF TEXTILES OR THE LIKE; LAUNDERING; FLEXIBLE MATERIALS NOT OTHERWISE PROVIDED FOR
    • D06M—TREATMENT, NOT PROVIDED FOR ELSEWHERE IN CLASS D06, OF FIBRES, THREADS, YARNS, FABRICS, FEATHERS OR FIBROUS GOODS MADE FROM SUCH MATERIALS
    • D06M15/00—Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment
    • D06M15/19—Treating fibres, threads, yarns, fabrics, or fibrous goods made from such materials, with macromolecular compounds; Such treatment combined with mechanical treatment with synthetic macromolecular compounds
    • D06M15/37—Macromolecular compounds obtained otherwise than by reactions only involving carbon-to-carbon unsaturated bonds
    • D06M15/55—Epoxy resins
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/249921—Web or sheet containing structurally defined element or component

Landscapes

  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Polymers & Plastics (AREA)
  • Engineering & Computer Science (AREA)
  • Organic Chemistry (AREA)
  • Health & Medical Sciences (AREA)
  • Medicinal Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Reinforced Plastic Materials (AREA)
  • Moulding By Coating Moulds (AREA)
  • Epoxy Resins (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)
DE200560005714 2004-07-27 2005-07-26 Kontinuierliches pultrusionsverfahren zur herstellung von hochleistungs-strukturprofilen Active DE602005005714T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP04017696 2004-07-27
EP20040017696 EP1621323A1 (de) 2004-07-27 2004-07-27 Kontinuierliches Pultrusionsverfahren zur Herstellung von Tragprofilen mit hoher Leistungsfähigkeit
PCT/EP2005/008114 WO2006010592A1 (en) 2004-07-27 2005-07-26 Continuous pultrusion process for producing high performance structural profiles

Publications (2)

Publication Number Publication Date
DE602005005714D1 true DE602005005714D1 (de) 2008-05-08
DE602005005714T2 DE602005005714T2 (de) 2008-07-17

Family

ID=34925943

Family Applications (1)

Application Number Title Priority Date Filing Date
DE200560005714 Active DE602005005714T2 (de) 2004-07-27 2005-07-26 Kontinuierliches pultrusionsverfahren zur herstellung von hochleistungs-strukturprofilen

Country Status (7)

Country Link
US (1) US7867568B2 (de)
EP (2) EP1621323A1 (de)
JP (1) JP4762239B2 (de)
AT (1) ATE390267T1 (de)
DE (1) DE602005005714T2 (de)
ES (1) ES2301039T3 (de)
WO (1) WO2006010592A1 (de)

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US8034453B2 (en) * 2008-10-07 2011-10-11 Hexcel Corporation Composite materials with improved burn properties
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AT514342A1 (de) 2013-05-17 2014-12-15 Asamer Basaltic Fibers Gmbh Verfahren zur Herstellung eines Bewehrungsstabes
DE102013226753A1 (de) 2013-12-19 2015-06-25 Airbus Operations Gmbh Vorrichtung und Verfahren zur kontinuierlichen Fertigung von Strukturbauteilen aus faserverstärkten Verbundmaterialien sowie Formwerkzeugset
DE102013226739A1 (de) 2013-12-19 2015-06-25 Airbus Operations Gmbh Formwerkzeug, Formgebungseinrichtung und Verfahren zum Verformen eines Verstärkungsfasern enthaltenden Halbzeugs
DE102013226730A1 (de) 2013-12-19 2015-07-09 Airbus Operations Gmbh Imprägnierwerkzeug und Verfahren zum kontinuierlichen Imprägnieren eines Verstärkungsfasermaterials mit einem Kunststoffmaterial
FR3020780B1 (fr) * 2014-05-09 2017-01-13 Airbus Operations Sas Procede de fabrication d'une piece en materiau composite pour structure d'aeronef par pultrusion et cocuisson
US10253142B2 (en) 2014-10-21 2019-04-09 Toray Industries, Inc. Epoxy resin composition and fiber reinforced composite material
DE102014222846A1 (de) * 2014-11-10 2016-05-12 Volkswagen Aktiengesellschaft Verfahren zum mittels Pultrusion Herstellen von Faserverbundstoffprofilteilen sowie Faserverbundstoffprofilteil
US20170247502A1 (en) 2014-11-20 2017-08-31 Dow Global Technologies Llc Curable Epoxy Composition Including Accelerator
DE102015211670A1 (de) 2015-06-24 2016-12-29 Airbus Operations Gmbh Verfahren und Vorrichtung zur Serienfertigung von Bauteilen aus einem faserverstärkten Verbundmaterial
EP3315530B1 (de) 2015-06-25 2022-12-21 Toray Industries, Inc. Epoxidharzzusammensetzung, faserverstärktes verbundmaterial, formartikel und druckbehälter
CN105729832A (zh) * 2016-04-01 2016-07-06 安徽冠廷科技有限公司 一种碳纤维复合工字钢的生产工艺
CN105835379A (zh) * 2016-04-01 2016-08-10 安徽冠廷科技有限公司 一种玻璃纤维复合型材的生产工艺
CN105729744A (zh) * 2016-04-01 2016-07-06 安徽冠廷科技有限公司 一种碳纤维复合t型钢的生产工艺
CN109415495B (zh) 2016-07-25 2020-09-11 东丽株式会社 预浸料坯及纤维增强复合材料
JP6462190B2 (ja) * 2016-07-28 2019-01-30 帝人株式会社 プレス成形品の製造方法
DE102016214654A1 (de) 2016-08-08 2018-02-08 Airbus Operations Gmbh Technik zur kontinuierlichen Fertigung von Bauteilen mit faserverstärkten Verbundmaterialien
FR3068284B1 (fr) * 2017-06-30 2021-09-10 Airbus Group Sas Procede de fabrication de pieces composites thermodurcissables par formage de preformes fibreuses injectees ou infusees
CN111655766B (zh) 2018-01-31 2022-11-22 东丽株式会社 纤维增强成型品及其制造方法
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CN114786928A (zh) * 2019-11-12 2022-07-22 内乌沃卡斯公司 一种生产复合材料的方法
WO2022009628A1 (ja) * 2020-07-08 2022-01-13 味の素株式会社 エポキシ樹脂用硬化剤
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Also Published As

Publication number Publication date
US20080145634A1 (en) 2008-06-19
ES2301039T3 (es) 2008-06-16
EP1819503B1 (de) 2008-03-26
DE602005005714T2 (de) 2008-07-17
WO2006010592A1 (en) 2006-02-02
JP4762239B2 (ja) 2011-08-31
JP2008508113A (ja) 2008-03-21
EP1819503A1 (de) 2007-08-22
ATE390267T1 (de) 2008-04-15
US7867568B2 (en) 2011-01-11
EP1621323A1 (de) 2006-02-01

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Owner name: AIRBUS OPERATIONS GMBH, 21129 HAMBURG, DE