Movatterモバイル変換


[0]ホーム

URL:


GB8927734D0 - A composite material - Google Patents

A composite material

Info

Publication number
GB8927734D0
GB8927734D0GB898927734AGB8927734AGB8927734D0GB 8927734 D0GB8927734 D0GB 8927734D0GB 898927734 AGB898927734 AGB 898927734AGB 8927734 AGB8927734 AGB 8927734AGB 8927734 D0GB8927734 D0GB 8927734D0
Authority
GB
United Kingdom
Prior art keywords
vacuum bag
stacks
composite material
mould
stack
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.)
Pending
Application number
GB898927734A
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 PLCfiledCriticalShort Brothers PLC
Priority to GB898927734ApriorityCriticalpatent/GB8927734D0/en
Publication of GB8927734D0publicationCriticalpatent/GB8927734D0/en
Priority to GB9026576Aprioritypatent/GB2238977B/en
Priority to BR909007901Aprioritypatent/BR9007901A/en
Priority to PCT/GB1990/001903prioritypatent/WO1991008892A1/en
Priority to JP3501309Aprioritypatent/JPH05501994A/en
Priority to AU69079/91Aprioritypatent/AU6907991A/en
Priority to EP91900894Aprioritypatent/EP0504247A1/en
Priority to CA002070830Aprioritypatent/CA2070830A1/en
Priority to IL96596Aprioritypatent/IL96596A0/en
Priority to FI922471Aprioritypatent/FI922471A0/en
Pendinglegal-statusCriticalCurrent

Links

Classifications

Landscapes

Abstract

A composite material is manufactured from two spaced stacks (2 and 4) of intermediate fabric material. Each stack consists of a plurality of layers of material placed together face to face. Each layer is formed by embedding high strength fibres having a high modulus of elasticity in a resin matrix. The stacks (2 and 4) are removed from a release film (6), and a film of adhesive is applied to the lower surface of the side portion (8) of the stack (2) and the upper surface of the side portion (10) of the stack (4). These side portions (8 and 10) are placed in overlapping relationship, and are then crimp fastened together by a plurality of fasteners (12). Further layers (14 and 16) of intermediate fabric material are placed over the side portions (8 and 10) to cover the fasteners (12). The crimp fastened stacks (2 and 4) are placed in a mould tool comprising a base plate (18) and a top mould plate (20). A vacuum bag (22) is placed over the top mould plate (20), and an air tight seal is made between the vacuum bag (22) and the base plate (18) by means of a peripheral sealer tape (24). The space inside the vacuum bag (22) is evacuated by withdrawing air through a passage (34) at one edge of the vacuum bag (22). The fastened stacks (2 and 4) are compressed by bringing together the plates (18 and 20), and the mould tool and vacuum bag assembly is then heated in an autoclave to cure the stacks (2 and 4) while they remain under pressure to form the required composite material. After the curing operation has been completed, the mould tool and vacuum bag assembly is removed from the autoclave, the vacuum bag (22) is removed, the mould plates (18 and 20) are separated, and the cured composite material is removed.
GB898927734A1989-12-071989-12-07A composite materialPendingGB8927734D0 (en)

Priority Applications (10)

Application NumberPriority DateFiling DateTitle
GB898927734AGB8927734D0 (en)1989-12-071989-12-07A composite material
CA002070830ACA2070830A1 (en)1989-12-071990-12-06Composite material
JP3501309AJPH05501994A (en)1989-12-071990-12-06 composite material
BR909007901ABR9007901A (en)1989-12-071990-12-06 PROCESS OF MANUFACTURING A COMPOSITE MATERIAL AND COMPOSITE MATERIAL MANUFACTURED BY THE PROCESS
PCT/GB1990/001903WO1991008892A1 (en)1989-12-071990-12-06A composite material
GB9026576AGB2238977B (en)1989-12-071990-12-06A composite material
AU69079/91AAU6907991A (en)1989-12-071990-12-06A composite material
EP91900894AEP0504247A1 (en)1989-12-071990-12-06A composite material
IL96596AIL96596A0 (en)1989-12-071990-12-07Method of manufacturing composite material and material produced thereby
FI922471AFI922471A0 (en)1989-12-071992-05-29 KOMBINERINGSMATERIAL.

Applications Claiming Priority (1)

Application NumberPriority DateFiling DateTitle
GB898927734AGB8927734D0 (en)1989-12-071989-12-07A composite material

Publications (1)

Publication NumberPublication Date
GB8927734D0true GB8927734D0 (en)1990-02-07

Family

ID=10667605

Family Applications (2)

Application NumberTitlePriority DateFiling Date
GB898927734APendingGB8927734D0 (en)1989-12-071989-12-07A composite material
GB9026576AExpired - Fee RelatedGB2238977B (en)1989-12-071990-12-06A composite material

Family Applications After (1)

Application NumberTitlePriority DateFiling Date
GB9026576AExpired - Fee RelatedGB2238977B (en)1989-12-071990-12-06A composite material

Country Status (9)

CountryLink
EP (1)EP0504247A1 (en)
JP (1)JPH05501994A (en)
AU (1)AU6907991A (en)
BR (1)BR9007901A (en)
CA (1)CA2070830A1 (en)
FI (1)FI922471A0 (en)
GB (2)GB8927734D0 (en)
IL (1)IL96596A0 (en)
WO (1)WO1991008892A1 (en)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
ES2213390T5 (en)1998-05-202008-12-16Cytec Technology Corp. MANUFACTURE OF LAMINATES FREE OF POROSITY AND USE OF THE SAME.
US8444087B2 (en)*2005-04-282013-05-21The Boeing CompanyComposite skin and stringer structure and method for forming the same
US7740932B2 (en)2005-03-312010-06-22The Boeing CompanyHybrid fiberglass composite structures and methods of forming the same
US8720825B2 (en)2005-03-312014-05-13The Boeing CompanyComposite stiffeners for aerospace vehicles
US7467763B2 (en)2005-06-032008-12-23Kismarton Max UComposite landing gear apparatus and methods
US7721495B2 (en)2005-03-312010-05-25The Boeing CompanyComposite structural members and methods for forming the same
US7748119B2 (en)2005-06-032010-07-06The Boeing CompanyMethod for manufacturing composite components
DE102006001494B3 (en)*2006-01-112007-08-02Airbus Deutschland GmbhMethod for producing bond of aircraft components involves covering electrical heating film and aircraft components, by cover sealingly connected with surface of aircraft component, to form cavity
GB0619667D0 (en)2006-10-052006-11-15Short Brothers LtdApparatus and method for close tolerance forming of areas in fibre reinforced resin composite components
DE102008039223B8 (en)*2008-08-222010-06-10Deutsches Zentrum für Luft- und Raumfahrt e.V. Fiber composite structure and manufacturing method therefor
DE102009010292A1 (en)*2009-02-242010-08-26Bayerische Motoren Werke Aktiengesellschaft Process for producing a fiber-reinforced plastic component
GB2475523B (en)*2009-11-202012-09-05Gkn Aerospace Services LtdDual-skin structures
JPWO2011105540A1 (en)*2010-02-262013-06-20三菱重工業株式会社 Composite repair method and composite material using the same
DE102011006792B4 (en)*2011-04-052017-07-27Airbus Operations Gmbh Method for producing and connecting fiber-reinforced components as well as aircraft or spacecraft
US8940222B2 (en)2011-11-032015-01-27The Boeing CompanyHigh flow edge breather and method
DE102011120636A1 (en)2011-12-092013-06-13Airbus Operations Gmbh Fiber composite component assembly having at least two plate-shaped fiber composite components and method for producing the same
FR2998210B1 (en)*2012-11-202017-03-10Plastic Omnium Cie ASSEMBLY OF A METAL INSERT AND A MATERIAL COMPOSITE TABLE, METHOD FOR INCORPORATING SUCH AN INSERT IN SUCH A TABLET AND PART OBTAINED BY MOLDING SUCH A TABLET
US9878773B2 (en)2012-12-032018-01-30The Boeing CompanySplit resistant composite laminate
US9610728B2 (en)*2014-07-182017-04-04The Boeing CompanyApparatus and methods for bonding laminate structures
US10457017B2 (en)2014-12-082019-10-29The Boeing CompanyMethod of forming a layered composite assembly
AT516904A1 (en)*2015-03-052016-09-15Engel Austria Gmbh Fiber composite component and method of manufacture
EP3498448B1 (en)2016-08-092021-11-24Nissan Motor Co., Ltd.Molding method for composite material and intermediate member for composite material
FR3056145B1 (en)*2016-09-162018-10-26Plastic Omnium Cie IMPROVED MANUFACTURING METHOD OF A HYBRID STRUCTURE OF A MOTOR VEHICLE AND CORRESPONDING HYBRID STRUCTURE PIECE
US20210122126A1 (en)*2017-03-102021-04-29Mitsubishi Heavy Industries, Ltd.Composite material pressurizing device and composite material forming method
CN109720415B (en)*2017-10-272022-07-15全耐塑料公司 Manufacturing method of improved motor vehicle hybrid structural component and corresponding hybrid structural component
DE102017125621A1 (en)*2017-11-022019-05-02Deutsches Zentrum für Luft- und Raumfahrt e.V. Connecting element for fiber composite components, method for connecting fiber composite components, apparatus for connecting fiber composite components and fiber composite component assembly
CN108297458B (en)*2018-04-042023-05-02吉林大学Forming and riveting method for carbon fiber composite material and metal plate
CN108943761B (en)*2018-06-212020-06-02江西昌河航空工业有限公司Curing method for steel mesh and skin of engine nozzle
CN111746000B (en)*2020-06-162022-07-29上海复合材料科技有限公司Strake slender composite material wing surface and forming method thereof
CN114055806B (en)*2021-10-262022-08-12成都飞机工业(集团)有限责任公司Composite material hybrid skin forming method

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
GB841371A (en)*1957-08-131960-07-13Aeroplastics LtdImprovements relating to methods of manufacturing hollow bodies of synthetic-resin-impregnated glass fibre
FR2312369A1 (en)*1975-05-261976-12-24Dassault Avions POROUS STRUCTURE
DE3246803A1 (en)*1982-12-171984-06-20Messerschmitt-Bölkow-Blohm GmbH, 8000 München METHOD FOR PRODUCING COMPONENTS FROM LAYERS OF FIBER REINFORCED PLASTIC
US4717302A (en)*1984-06-181988-01-05Tiodize Company, Inc.Composite fastener
US4786343A (en)*1985-05-101988-11-22The Boeing CompanyMethod of making delamination resistant composites
US4679291A (en)*1986-02-261987-07-14Shell Oil CompanyRobotic stapling system for fiber placement for composite parts
US4808461A (en)*1987-12-141989-02-28Foster-Miller, Inc.Composite structure reinforcement

Also Published As

Publication numberPublication date
BR9007901A (en)1992-09-22
WO1991008892A1 (en)1991-06-27
JPH05501994A (en)1993-04-15
AU6907991A (en)1991-07-18
GB9026576D0 (en)1991-01-23
EP0504247A1 (en)1992-09-23
FI922471A7 (en)1992-05-29
GB2238977B (en)1994-01-05
CA2070830A1 (en)1991-06-08
GB2238977A (en)1991-06-19
IL96596A0 (en)1991-09-16
FI922471A0 (en)1992-05-29

Similar Documents

PublicationPublication DateTitle
GB2238977B (en)A composite material
US5108532A (en)Method and apparatus for shaping, forming, consolidating and co-consolidating thermoplastic or thermosetting composite products
US4869770A (en)Method and apparatus for laminating composite materials
US4816106A (en)Method for the controlled curing of composites
US5366684A (en)Molding composite method using an inflatable bladder pressurized in an autoclave
JP3403201B2 (en) Manufacturing method of honeycomb core composite product
EP0585545B1 (en)A breather pad mainly made out of nylon fibers
GB2168002A (en)Composite material manufacture
US4963215A (en)Method for debulking precured thermoplastic composite laminae
US3996091A (en)Method and apparatus for heat bonding
JPH02175238A (en)Method for continuously molding honeycomb panel
CA2245088C (en)Method for forming inner mold line tooling without a part model
CA2201981A1 (en)Dual purpose lay-up tool
EP0175510B1 (en)Vacuum bagging
US4708758A (en)Method of making a flexible bearing
US6350115B1 (en)Pressure transmitters for use in the production of composite components
EP0319895A2 (en)Method for debulking partially precured thermoplastic composite laminae
EP0355641A2 (en)Laminating tool and method
US7306761B2 (en)Method of manufacturing composite sandwich structures
CN117400560A (en)Forming method of cap-shaped stringer co-glued wallboard
JP3204529B2 (en) Method for manufacturing curved honeycomb panel
JP2685554B2 (en) Method for manufacturing a slab laminate with a composite material
US2472023A (en)Method of forming wood assemblies
JP2002240151A (en)Method and apparatus for manufacturing fiberboard having decorative film laminated thereto
AU2002328694B2 (en)Method of manufacturing composite sandwich structures

[8]ページ先頭

©2009-2025 Movatter.jp