ATE482808T1 - Verfahren und formkern zur herstellung einer faserverbundkomponente für luft- und raumfahrt - Google Patents

Verfahren und formkern zur herstellung einer faserverbundkomponente für luft- und raumfahrt

Info

Publication number
ATE482808T1
ATE482808T1 AT07787084T AT07787084T ATE482808T1 AT E482808 T1 ATE482808 T1 AT E482808T1 AT 07787084 T AT07787084 T AT 07787084T AT 07787084 T AT07787084 T AT 07787084T AT E482808 T1 ATE482808 T1 AT E482808T1
Authority
AT
Austria
Prior art keywords
layup
form core
tubes
aerospace
curing
Prior art date
Application number
AT07787084T
Other languages
English (en)
Inventor
Torben Jacob
Joachim Piepenbrock
Original Assignee
Airbus 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 Airbus Gmbh filed Critical Airbus Gmbh
Priority claimed from PCT/EP2007/056788 external-priority patent/WO2008003733A1/en
Application granted granted Critical
Publication of ATE482808T1 publication Critical patent/ATE482808T1/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
    • 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
    • B29C33/48—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 with means for collapsing or disassembling
    • B29C33/50—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 with means for collapsing or disassembling elastic or flexible
    • B29C33/505—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 with means for collapsing or disassembling elastic or flexible cores or mandrels, e.g. inflatable
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
    • 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
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628—Nonplanar uniform thickness material
    • Y10T428/24661—Forming, or cooperating to form cells

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Architecture (AREA)
  • Civil Engineering (AREA)
  • Structural Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
AT07787084T 2006-07-06 2007-07-05 Verfahren und formkern zur herstellung einer faserverbundkomponente für luft- und raumfahrt ATE482808T1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US81893206P 2006-07-06 2006-07-06
DE102006031334A DE102006031334A1 (de) 2006-07-06 2006-07-06 Verfahren zur Herstellung eines Faserverbundbauteils für die Luft- und Raumfahrt
PCT/EP2007/056788 WO2008003733A1 (en) 2006-07-06 2007-07-05 Method and moulding core for producing a fibre composite component for aviation and spaceflight and fibre composite component obtained thereby

Publications (1)

Publication Number Publication Date
ATE482808T1 true ATE482808T1 (de) 2010-10-15

Family

ID=38806034

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07787084T ATE482808T1 (de) 2006-07-06 2007-07-05 Verfahren und formkern zur herstellung einer faserverbundkomponente für luft- und raumfahrt

Country Status (6)

Country Link
US (1) US8906489B2 (de)
CN (1) CN101484290B (de)
AT (1) ATE482808T1 (de)
BR (1) BRPI0714226A2 (de)
DE (2) DE102006031334A1 (de)
RU (1) RU2438866C2 (de)

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BRPI0714226A2 (pt) 2013-10-29
RU2009103204A (ru) 2010-08-20
CN101484290A (zh) 2009-07-15
US20110076461A1 (en) 2011-03-31
US8906489B2 (en) 2014-12-09
RU2438866C2 (ru) 2012-01-10
CN101484290B (zh) 2012-06-27

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