ATE228058T1 - Verfahren zur herstellung eines mit gefüllten hohlfasern versehenen verbundmaterials - Google Patents

Verfahren zur herstellung eines mit gefüllten hohlfasern versehenen verbundmaterials

Info

Publication number
ATE228058T1
ATE228058T1 AT00942225T AT00942225T ATE228058T1 AT E228058 T1 ATE228058 T1 AT E228058T1 AT 00942225 T AT00942225 T AT 00942225T AT 00942225 T AT00942225 T AT 00942225T AT E228058 T1 ATE228058 T1 AT E228058T1
Authority
AT
Austria
Prior art keywords
hollow fibre
plies
composite material
film material
interleaved
Prior art date
Application number
AT00942225T
Other languages
English (en)
Inventor
Michael Dunleavy
Christopher Somerton
Charfield Newtown
Jennifer Hudd
Sajad Haq
Original Assignee
Bae Systems Plc
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 Bae Systems Plc filed Critical Bae Systems Plc
Application granted granted Critical
Publication of ATE228058T1 publication Critical patent/ATE228058T1/de

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
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • 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
    • B29C70/545—Perforating, cutting or machining during or after 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/11—Methods of delaminating, per se; i.e., separating at bonding face

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Laminated Bodies (AREA)
  • Reinforced Plastic Materials (AREA)
  • Spinning Methods And Devices For Manufacturing Artificial Fibers (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Multicomponent Fibers (AREA)
  • Peptides Or Proteins (AREA)
  • Separation Using Semi-Permeable Membranes (AREA)
  • Moulding By Coating Moulds (AREA)
AT00942225T 1999-07-10 2000-06-29 Verfahren zur herstellung eines mit gefüllten hohlfasern versehenen verbundmaterials ATE228058T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9916157.2A GB9916157D0 (en) 1999-07-10 1999-07-10 Method for manufacturing a filled hollow fibre composite mate rial
PCT/GB2000/002506 WO2001003910A1 (en) 1999-07-10 2000-06-29 Method for manufacturing a filled hollow fibre composite material

Publications (1)

Publication Number Publication Date
ATE228058T1 true ATE228058T1 (de) 2002-12-15

Family

ID=10856982

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00942225T ATE228058T1 (de) 1999-07-10 2000-06-29 Verfahren zur herstellung eines mit gefüllten hohlfasern versehenen verbundmaterials

Country Status (12)

Country Link
US (1) US6478913B1 (de)
EP (1) EP1194282B8 (de)
JP (1) JP3542794B2 (de)
AT (1) ATE228058T1 (de)
AU (1) AU764873B2 (de)
CA (1) CA2378164C (de)
DE (1) DE60000834T2 (de)
ES (1) ES2182808T3 (de)
GB (1) GB9916157D0 (de)
NO (1) NO20020063L (de)
WO (1) WO2001003910A1 (de)
ZA (1) ZA200200226B (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111086234A (zh) * 2019-12-12 2020-05-01 北京汽车集团有限公司 热塑性复合材料和复合材料部件及其制造方法

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6527849B2 (en) * 1990-06-19 2003-03-04 Carolyn M. Dry Self-repairing, reinforced matrix materials
CA2615699A1 (en) 2005-07-01 2007-01-11 Carolyn M. Dry Multiple function, self-repairing composites with special adhesives
JP5533743B2 (ja) * 2010-09-24 2014-06-25 東レ株式会社 繊維強化プラスチックの製造方法
FR2991228B1 (fr) 2012-05-29 2015-03-06 Airbus Operations Sas Procede et dispositif de realisation d'un panneau composite auto-raidi
FR2999970B1 (fr) * 2012-12-20 2015-06-19 Airbus Operations Sas Procede de realisation d'une preforme textile a fibres continues par circulation d'un flux de gaz chaud a travers un ensemble fibreux
US10212812B2 (en) * 2016-01-15 2019-02-19 International Business Machines Corporation Composite materials including filled hollow glass filaments
US9863875B1 (en) * 2016-10-19 2018-01-09 International Business Machines Corporation In-situ detection of hollow glass fiber formation
DE102019203227A1 (de) * 2019-03-11 2020-09-17 Audi Ag Formwerkzeug zum Urformen oder Umformen eines Werkstücks mit einer Temperiereinrichtung

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5050523A (de) * 1973-09-07 1975-05-07
FR2549969B1 (fr) * 1983-07-27 1985-09-27 Cables De Lyon Geoffroy Delore Procede d'injection d'un produit de remplissage visqueux dans les rainures de logement des fibres optiques d'un jonc, et dispositif de mise en oeuvre de ce procede
US4851065A (en) * 1986-01-17 1989-07-25 Tyee Aircraft, Inc. Construction of hollow, continuously wound filament load-bearing structure
DE3839966A1 (de) * 1988-11-26 1990-05-31 Akzo Gmbh Hohlfadenmodul
DE4107618C2 (de) * 1991-03-09 1994-08-25 Deutsche Aerospace Faserverbundwerkstoff
DE4107617C2 (de) * 1991-03-09 1995-01-12 Deutsche Aerospace Faserverbundwerkstoff
JPH04310222A (ja) * 1991-04-08 1992-11-02 Asahi Chem Ind Co Ltd 複合中空糸膜の製造法
JPH10225533A (ja) * 1997-02-13 1998-08-25 Kasco Corp ゴルフボール

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111086234A (zh) * 2019-12-12 2020-05-01 北京汽车集团有限公司 热塑性复合材料和复合材料部件及其制造方法

Also Published As

Publication number Publication date
DE60000834D1 (de) 2003-01-02
EP1194282B8 (de) 2003-03-05
EP1194282B1 (de) 2002-11-20
WO2001003910A1 (en) 2001-01-18
AU764873B2 (en) 2003-09-04
CA2378164A1 (en) 2001-01-18
JP2003504234A (ja) 2003-02-04
EP1194282A1 (de) 2002-04-10
CA2378164C (en) 2006-05-16
DE60000834T2 (de) 2003-03-27
AU5693000A (en) 2001-01-30
JP3542794B2 (ja) 2004-07-14
ES2182808T3 (es) 2003-03-16
US6478913B1 (en) 2002-11-12
ZA200200226B (en) 2003-03-26
NO20020063L (no) 2002-02-14
GB9916157D0 (en) 1999-09-08
NO20020063D0 (no) 2002-01-07

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