DE60310613D1 - Verfahren zur herstellung eines laminats aus metallschichten und faserverstärkten kunststoffschichten - Google Patents

Verfahren zur herstellung eines laminats aus metallschichten und faserverstärkten kunststoffschichten

Info

Publication number
DE60310613D1
DE60310613D1 DE60310613T DE60310613T DE60310613D1 DE 60310613 D1 DE60310613 D1 DE 60310613D1 DE 60310613 T DE60310613 T DE 60310613T DE 60310613 T DE60310613 T DE 60310613T DE 60310613 D1 DE60310613 D1 DE 60310613D1
Authority
DE
Germany
Prior art keywords
layers
laminate
fiber
producing
reinforced plastic
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.)
Expired - Fee Related
Application number
DE60310613T
Other languages
English (en)
Other versions
DE60310613T2 (de
Inventor
Faziel Rajabali
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.)
GKN Fokker Aerospace BV
Original Assignee
Stork Fokker AESP BV
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 Stork Fokker AESP BV filed Critical Stork Fokker AESP BV
Application granted granted Critical
Publication of DE60310613D1 publication Critical patent/DE60310613D1/de
Publication of DE60310613T2 publication Critical patent/DE60310613T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B15/00—Layered products comprising a layer of metal
    • B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
    • B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
    • 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
    • B29C70/08—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • B29C70/088—Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers and with one or more layers of non-plastics material or non-specified material, e.g. supports
    • 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
    • B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/18—Handling of layers or the laminate
    • B32B38/1825—Handling of layers or the laminate characterised by the control or constructional features of devices for tensioning, stretching or registration
    • B32B38/1833—Positioning, e.g. registration or centering
    • B32B38/1841—Positioning, e.g. registration or centering during laying up
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/08—Reinforcements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2311/00—Metals, their alloys or their compounds
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2607/00—Walls, panels
    • 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

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
DE60310613T 2002-11-06 2003-11-06 Verfahren zur herstellung eines laminats aus metallschichten und faserverstärkten kunststoffschichten Expired - Fee Related DE60310613T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
NL1021860A NL1021860C2 (nl) 2002-11-06 2002-11-06 Werkwijze voor het vervaardigen van een laminaat.
NL1021860 2002-11-06
PCT/NL2003/000775 WO2004041519A1 (en) 2002-11-06 2003-11-06 Method for production of a laminate from metal layers and fibre reinforced plastic layers

Publications (2)

Publication Number Publication Date
DE60310613D1 true DE60310613D1 (de) 2007-02-01
DE60310613T2 DE60310613T2 (de) 2007-09-27

Family

ID=32310923

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60310613T Expired - Fee Related DE60310613T2 (de) 2002-11-06 2003-11-06 Verfahren zur herstellung eines laminats aus metallschichten und faserverstärkten kunststoffschichten

Country Status (11)

Country Link
US (1) US20060011294A1 (de)
EP (1) EP1578592B1 (de)
JP (1) JP2006515236A (de)
CN (1) CN1735501A (de)
AU (1) AU2003280895A1 (de)
BR (1) BR0316058A (de)
CA (1) CA2505331A1 (de)
DE (1) DE60310613T2 (de)
NL (1) NL1021860C2 (de)
RU (1) RU2323090C2 (de)
WO (1) WO2004041519A1 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2003269656A1 (en) * 2003-09-18 2005-04-06 Avestor Limited Partnership Stacking apparatus and method for assembly of polymer batteries
GB0614087D0 (en) 2006-07-14 2006-08-23 Airbus Uk Ltd Composite manufacturing method
GB0619667D0 (en) 2006-10-05 2006-11-15 Short Brothers Ltd Apparatus and method for close tolerance forming of areas in fibre reinforced resin composite components
GB2453308B (en) * 2007-10-03 2012-07-25 Acell Group Ltd Composite products
US9656450B2 (en) 2008-01-02 2017-05-23 Tpk Touch Solutions, Inc. Apparatus for laminating substrates
GB201116472D0 (en) * 2011-09-23 2011-11-09 Hexcel Composites Ltd Conductive composite structure or laminate
CN103203882A (zh) * 2013-02-27 2013-07-17 哈尔滨飞机工业集团有限责任公司 一种预浸玻璃布试片毛坯固化前封装方法
WO2015066546A1 (en) * 2013-10-31 2015-05-07 Rodman William L Composite structures having embedded mechanical features
GB2535193A (en) * 2015-02-12 2016-08-17 Zodiac Seats Uk Ltd Tool for curing a composite component
US11046034B2 (en) * 2016-04-18 2021-06-29 Rohr, Inc. Manufacturing a fiber-reinforced composite component using mandrels
US11185966B2 (en) * 2017-02-06 2021-11-30 The Boeing Company Hybrid tool pins
CN114502360A (zh) * 2019-06-07 2022-05-13 泰普爱复合材料股份有限公司 用于风力涡轮机叶片的制造期间的部件定位的模具精密销

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0443020A (ja) * 1990-06-08 1992-02-13 Yotaro Hatamura 積層基板圧着方法および装置
WO1996022878A1 (en) * 1995-01-27 1996-08-01 Sikorsky Aircraft Corporation Method for making honeycomb core composite articles

Also Published As

Publication number Publication date
CA2505331A1 (en) 2004-05-21
JP2006515236A (ja) 2006-05-25
NL1021860C2 (nl) 2004-05-07
WO2004041519A1 (en) 2004-05-21
DE60310613T2 (de) 2007-09-27
AU2003280895A1 (en) 2004-06-07
RU2323090C2 (ru) 2008-04-27
CN1735501A (zh) 2006-02-15
US20060011294A1 (en) 2006-01-19
EP1578592A1 (de) 2005-09-28
BR0316058A (pt) 2005-09-27
EP1578592B1 (de) 2006-12-20
RU2005117152A (ru) 2006-01-20

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee