AU7487991A - Structural component - Google Patents

Structural component

Info

Publication number
AU7487991A
AU7487991A AU74879/91A AU7487991A AU7487991A AU 7487991 A AU7487991 A AU 7487991A AU 74879/91 A AU74879/91 A AU 74879/91A AU 7487991 A AU7487991 A AU 7487991A AU 7487991 A AU7487991 A AU 7487991A
Authority
AU
Australia
Prior art keywords
mandrels
core
assembly
mandrel
core material
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.)
Abandoned
Application number
AU74879/91A
Other languages
English (en)
Inventor
Derek James Simpson
Robert Samuel Wilson
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.)
Short Brothers PLC
Original Assignee
Short Brothers 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 Short Brothers PLC filed Critical Short Brothers PLC
Publication of AU7487991A publication Critical patent/AU7487991A/en
Abandoned legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/001Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
    • B29D99/0021Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with plain or filled structures, e.g. cores, placed between two or more plates or sheets, e.g. in a matrix
    • 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
    • B29C70/34Shaping 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
    • 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
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • 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
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • 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
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/10Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
    • B29C43/12Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material
    • 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

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)
  • Laminated Bodies (AREA)
  • Glass Compositions (AREA)
  • Piezo-Electric Transducers For Audible Bands (AREA)
AU74879/91A 1990-03-21 1991-03-20 Structural component Abandoned AU7487991A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB909006358A GB9006358D0 (en) 1990-03-21 1990-03-21 Structural component
GB9006358 1990-03-21

Publications (1)

Publication Number Publication Date
AU7487991A true AU7487991A (en) 1991-10-21

Family

ID=10672999

Family Applications (1)

Application Number Title Priority Date Filing Date
AU74879/91A Abandoned AU7487991A (en) 1990-03-21 1991-03-20 Structural component

Country Status (7)

Country Link
EP (1) EP0473751A1 (de)
AU (1) AU7487991A (de)
BR (1) BR9105098A (de)
CA (1) CA2058297A1 (de)
GB (2) GB9006358D0 (de)
IL (1) IL97589A0 (de)
WO (1) WO1991014565A1 (de)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5190773A (en) * 1991-11-18 1993-03-02 United Technologies Corporation Mold for fabricating composite articles having integrally bonded stiffening members
US20020090874A1 (en) * 2000-09-08 2002-07-11 Mckague Elbert L. Unitized fastenerless composite structure
FR2818578B1 (fr) * 2000-12-26 2003-03-21 Snecma Moteurs Procede de fabrication de structures en nid d'abeilles et outillage pour une telle fabrication
GB0213161D0 (en) * 2002-06-07 2002-07-17 Short Brothers Plc A fibre reinforced composite component
US8323549B2 (en) 2008-11-17 2012-12-04 Textron Systems Corporation Techniques for forming temporary protective coatings and bondable surfaces
FR2949710B1 (fr) * 2009-09-04 2011-11-25 Lorraine Construction Aeronautique Dispositif de moulage destine a recevoir des fibres et une resine par injection.
GB201012293D0 (en) * 2010-07-22 2010-09-08 Advanced Composites Group Ltd Mould tools
US10272619B2 (en) 2014-05-19 2019-04-30 The Boeing Company Manufacture of a resin infused one-piece composite truss structure
US11673362B2 (en) * 2020-01-02 2023-06-13 The Boeing Company Composite structural panels and methods of forming thereof

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2125463A1 (en) * 1971-05-22 1972-12-14 Ferndorf Eisen Metall Plastic insulation panels - with honeycombed fibre glass reinforcing esp for boat and general construction
CA1166942A (en) * 1980-02-09 1984-05-08 Martin P. Ansell Cellular composites and process and apparatus for their manufacture
DE3315246C2 (de) * 1983-04-27 1986-05-07 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Bauteil in Sandwichbauweise
WO1987006186A1 (en) * 1986-04-11 1987-10-22 H R Smith (Technical Developments) Limited Lightweight high temperature thermoplastics material structures
DE3813237A1 (de) * 1988-04-20 1989-11-02 Wilhelmi Werke Gmbh & Co Kg Verfahren zur herstellung eines plattenfoermigen, schallabsorbierenden elements
GB2225742A (en) * 1988-12-09 1990-06-13 Westland Helicopters Moulding a fibre reinforced composite, into a hollow structure comprising outer and inner skins connected by ribs

Also Published As

Publication number Publication date
BR9105098A (pt) 1992-09-22
GB9105852D0 (en) 1991-05-08
GB9006358D0 (en) 1990-05-16
CA2058297A1 (en) 1991-09-22
IL97589A0 (en) 1992-06-21
WO1991014565A1 (en) 1991-10-03
EP0473751A1 (de) 1992-03-11
GB2242389A (en) 1991-10-02

Similar Documents

Publication Publication Date Title
US4492607A (en) Method for producing integrally stiffened fiber reinforced plastic panels
RU2469854C2 (ru) Способ изготовления монолитной структуры крыла с цельным профилем
EP0155820B2 (de) Formgebung von faserverstärkten Schichtstoffen
US5279892A (en) Composite airfoil with woven insert
US8007628B2 (en) Cellular composite grid-stiffened structure
US5346367A (en) Advanced composite rotor blade
US8236124B1 (en) Method for fabricating grid-stiffened composite structures
US5454895A (en) Process for manufacturing fiber reinforced structures suitable for aeronautic applications
US5344685A (en) Production of composite sandwich structures
EP1925436B1 (de) Herstellungsverfahren für einen faserverstärkten Schichtstoff, Verwendung dieses Schichtstoffes, Windturbinenschaufel und Windturbine mit solchem Schichtstoff
US4657615A (en) Composite leading edge/spar member for an aircraft control surface
EP2170587B1 (de) Verfahren zur herstellung eines gekrümmten elements aus einem verbundstoff
CA2172152A1 (en) A complex composite sandwich structure having a laminate disposed therein and a method for making the same
EP1791997B1 (de) Hochfestes verbindungssystem für faserverstärkte verbundwerkstoffe
AU7487991A (en) Structural component
US20210370620A1 (en) Semi-Finished Product And Method For Producing A Structural Component
EP0261902B1 (de) Verfahren zur Herstellung von vulkanisierten, laminierten, flexiblen Lagern
US4927481A (en) Method of making continuous reinforcement for flexible bearing laminate
JP4769252B2 (ja) 複合材製補強インサートの製造方法、およびそのようなインサートを備えるサンドイッチ構造の作製方法
EP0238628A4 (de) Giessvorrichtung unter verwendung von federn aus gedächtnismetall.
EP0337648A2 (de) Verfahren zum kontinuierlichen Verstärken von flexiblen lamellierten Lagern
SU1785910A1 (ru) Способ изготовления слоистой конструкции из композиционного материала и устройство для его осуществления
EP2582505B1 (de) Formwerkzeuge
WO2019245599A1 (en) Net edge composite core splices for aircraft wing
Elliott Chapter VI-Fabrication Processing