WO2008009988A3 - Composite structure and method of manufacture - Google Patents

Composite structure and method of manufacture Download PDF

Info

Publication number
WO2008009988A3
WO2008009988A3 PCT/GB2007/050401 GB2007050401W WO2008009988A3 WO 2008009988 A3 WO2008009988 A3 WO 2008009988A3 GB 2007050401 W GB2007050401 W GB 2007050401W WO 2008009988 A3 WO2008009988 A3 WO 2008009988A3
Authority
WO
WIPO (PCT)
Prior art keywords
internal elements
internal
manufacture
longitudinal
structural member
Prior art date
Application number
PCT/GB2007/050401
Other languages
French (fr)
Other versions
WO2008009988A2 (en
Inventor
John Yates
David Graham Inston
Original Assignee
Airbus Uk Ltd
John Yates
David Graham Inston
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 Uk Ltd, John Yates, David Graham Inston filed Critical Airbus Uk Ltd
Publication of WO2008009988A2 publication Critical patent/WO2008009988A2/en
Publication of WO2008009988A3 publication Critical patent/WO2008009988A3/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers
    • B64C3/187—Ribs
    • 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
    • B29C70/32—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 on a rotating mould, former or core
    • 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
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/84—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by moulding material on preformed parts to be joined
    • B29C70/845—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by moulding material on preformed parts to be joined by moulding material on a relative small portion of the preformed parts
    • 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
    • B29D22/00—Producing hollow articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • 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
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/80—Component parts, details or accessories; Auxiliary operations
    • B29C53/82—Cores or mandrels
    • B29C53/821—Mandrels especially adapted for winding and joining
    • B29C53/822—Single use mandrels, e.g. destructible, becoming part of the wound articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/748—Machines or parts thereof not otherwise provided for
    • 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)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Rod-Shaped Construction Members (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)

Abstract

A method of manufacture of a structural member comprising, providing a number of internal elements (16,18,20), each having an aperture formed therein, sequentially assembling the internal elements onto a longitudinal element (14) such that the longitudinal element passes through the aperture of each internal element, and wrapping an outer skin around the assembled internal elements and longitudinal element. A structural member is thus produced having a number of internal elements, each internal element having a longitudinal axis aligned with the longitudinal axis of the remaining internal elements, and having a continuous outer skin formed over the internal elements.
PCT/GB2007/050401 2006-07-20 2007-07-13 Composite structure and method of manufacture WO2008009988A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0614438.0 2006-07-20
GBGB0614438.0A GB0614438D0 (en) 2006-07-20 2006-07-20 Composite structure and method of manufacture

Publications (2)

Publication Number Publication Date
WO2008009988A2 WO2008009988A2 (en) 2008-01-24
WO2008009988A3 true WO2008009988A3 (en) 2009-01-22

Family

ID=36998429

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/GB2007/050401 WO2008009988A2 (en) 2006-07-20 2007-07-13 Composite structure and method of manufacture

Country Status (2)

Country Link
GB (1) GB0614438D0 (en)
WO (1) WO2008009988A2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102014106930B4 (en) 2014-05-16 2024-07-04 Airbus Operations Gmbh Load-bearing fairing element for a flap adjustment mechanism and aircraft with such a fairing element

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3074111A (en) * 1958-11-24 1963-01-22 White Sewing Machine Corp Apparatus for making a resin-bonded fiber glass cone
US4681724A (en) * 1986-04-28 1987-07-21 United Technologies Corporation Removable irreversibly shrinking male mandrel
WO2004076769A2 (en) * 2003-02-24 2004-09-10 Bell Helicopter Textron Inc. Contact stiffeners for structural skins

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3074111A (en) * 1958-11-24 1963-01-22 White Sewing Machine Corp Apparatus for making a resin-bonded fiber glass cone
US4681724A (en) * 1986-04-28 1987-07-21 United Technologies Corporation Removable irreversibly shrinking male mandrel
WO2004076769A2 (en) * 2003-02-24 2004-09-10 Bell Helicopter Textron Inc. Contact stiffeners for structural skins

Also Published As

Publication number Publication date
GB0614438D0 (en) 2006-08-30
WO2008009988A2 (en) 2008-01-24

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