ATE544672T1 - Längliche verbundstrukturelemente und verbesserungen davon - Google Patents

Längliche verbundstrukturelemente und verbesserungen davon

Info

Publication number
ATE544672T1
ATE544672T1 AT10172445T AT10172445T ATE544672T1 AT E544672 T1 ATE544672 T1 AT E544672T1 AT 10172445 T AT10172445 T AT 10172445T AT 10172445 T AT10172445 T AT 10172445T AT E544672 T1 ATE544672 T1 AT E544672T1
Authority
AT
Austria
Prior art keywords
spar
web
length
linearly
wing
Prior art date
Application number
AT10172445T
Other languages
English (en)
Inventor
Ian L Gray
Original Assignee
Airbus Operations Ltd
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 Operations Ltd filed Critical Airbus Operations Ltd
Application granted granted Critical
Publication of ATE544672T1 publication Critical patent/ATE544672T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping 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
    • B29C70/302Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064Stringers; Longerons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/065Spars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/182Stringers, longerons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/185Spars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/187Ribs
    • GPHYSICS
    • G06COMPUTING OR CALCULATING; COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/15Vehicle, aircraft or watercraft design
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/24Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
    • B29K2105/246Uncured, e.g. green
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0072Fuselage structures substantially made from particular materials from composite materials
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T90/00Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Composite Materials (AREA)
  • Chemical & Material Sciences (AREA)
  • Computational Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • General Engineering & Computer Science (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • Automation & Control Theory (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
AT10172445T 2007-06-29 2008-06-24 Längliche verbundstrukturelemente und verbesserungen davon ATE544672T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB0712552.9A GB0712552D0 (en) 2007-06-29 2007-06-29 Elongate composite structural members and improvements therein

Publications (1)

Publication Number Publication Date
ATE544672T1 true ATE544672T1 (de) 2012-02-15

Family

ID=38420865

Family Applications (2)

Application Number Title Priority Date Filing Date
AT10172445T ATE544672T1 (de) 2007-06-29 2008-06-24 Längliche verbundstrukturelemente und verbesserungen davon
AT08762589T ATE503685T1 (de) 2007-06-29 2008-06-24 Längliche verbundstrukturelemente und verbesserungen davon

Family Applications After (1)

Application Number Title Priority Date Filing Date
AT08762589T ATE503685T1 (de) 2007-06-29 2008-06-24 Längliche verbundstrukturelemente und verbesserungen davon

Country Status (12)

Country Link
US (1) US8864075B2 (de)
EP (2) EP2167379B1 (de)
JP (1) JP5686286B2 (de)
KR (2) KR101558988B1 (de)
CN (1) CN101772452B (de)
AT (2) ATE544672T1 (de)
BR (1) BRPI0813962A2 (de)
CA (1) CA2690988A1 (de)
DE (1) DE602008005884D1 (de)
GB (1) GB0712552D0 (de)
RU (1) RU2485011C2 (de)
WO (1) WO2009004363A2 (de)

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Also Published As

Publication number Publication date
EP2167379B1 (de) 2011-03-30
CA2690988A1 (en) 2009-01-08
KR101558988B1 (ko) 2015-10-19
RU2010102978A (ru) 2011-08-10
BRPI0813962A2 (pt) 2015-01-06
EP2243702A1 (de) 2010-10-27
CN101772452A (zh) 2010-07-07
JP2010531776A (ja) 2010-09-30
US20100170989A1 (en) 2010-07-08
JP5686286B2 (ja) 2015-03-18
RU2485011C2 (ru) 2013-06-20
WO2009004363A3 (en) 2009-05-14
DE602008005884D1 (de) 2011-05-12
KR20100040876A (ko) 2010-04-21
KR20150086382A (ko) 2015-07-27
ATE503685T1 (de) 2011-04-15
EP2243702B1 (de) 2012-02-08
KR101558987B1 (ko) 2015-10-12
EP2167379A2 (de) 2010-03-31
US8864075B2 (en) 2014-10-21
WO2009004363A2 (en) 2009-01-08
GB0712552D0 (en) 2007-08-08
CN101772452B (zh) 2013-05-08

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