GB1441919A - Production of fibre reinforced synthetic resin articles - Google Patents

Production of fibre reinforced synthetic resin articles

Info

Publication number
GB1441919A
GB1441919A GB3502672A GB3502672A GB1441919A GB 1441919 A GB1441919 A GB 1441919A GB 3502672 A GB3502672 A GB 3502672A GB 3502672 A GB3502672 A GB 3502672A GB 1441919 A GB1441919 A GB 1441919A
Authority
GB
United Kingdom
Prior art keywords
pressure
laminate
fibre
resin
synthetic resin
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.)
Expired
Application number
GB3502672A
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.)
Hawker Siddeley Aviation Ltd
Original Assignee
Hawker Siddeley Aviation 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 Hawker Siddeley Aviation Ltd filed Critical Hawker Siddeley Aviation Ltd
Priority to GB3502672A priority Critical patent/GB1441919A/en
Publication of GB1441919A publication Critical patent/GB1441919A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
    • B32B7/04—Interconnection of layers
    • B32B7/06—Interconnection of layers permitting easy separation
    • 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
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44—Shaping 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
    • B32B37/1018—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure using only vacuum
    • 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
    • B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
    • B29C43/12—Isostatic 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2305/00—Condition, form or state of the layers or laminate
    • B32B2305/08—Reinforcements
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2307/00—Properties of the layers or laminate
    • B32B2307/70—Other properties
    • B32B2307/748—Releasability

Abstract

1441919 Curing fibre-reinforced resin laminates HAWKER SIDDELEY AVIATION Ltd 26 July 1973 [26 July 1972] 35026/72 Heading B5N Fibre-reinforced synthetic resin laminates, e.g. carbon fibre/epoxy resin laminates, are cured under consolidating pressure which is applied to the exterior of a deformable chamber in which the laminate is sealed, the interior of the chamber having applied thereto a fluid pressure which is less than the external pressure but higher than the resin vapour pressure to prevent outgassing and consequent void formation. As shown, the laminate 11 is separated from bleeder layers 12 by release layers 13 and the assembly is covered by a flexible membrane 14 within which the fluid pressure is applied to the resin by a gas or liquid; the external pressure is applied outside the membrane by a press or autoclave. The laminate may be preheated at a temperature below the rapid gelation point whilst vented to atmosphere or to vacuum.
GB3502672A 1972-07-26 1972-07-26 Production of fibre reinforced synthetic resin articles Expired GB1441919A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3502672A GB1441919A (en) 1972-07-26 1972-07-26 Production of fibre reinforced synthetic resin articles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3502672A GB1441919A (en) 1972-07-26 1972-07-26 Production of fibre reinforced synthetic resin articles

Publications (1)

Publication Number Publication Date
GB1441919A true GB1441919A (en) 1976-07-07

Family

ID=10372923

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3502672A Expired GB1441919A (en) 1972-07-26 1972-07-26 Production of fibre reinforced synthetic resin articles

Country Status (1)

Country Link
GB (1) GB1441919A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2459118A1 (en) * 1979-06-18 1981-01-09 Poudres & Explosifs Ste Nale Moulding of fibre reinforced thermosetting prepregs - in heated autoclave, under flexible membrane, whilst passing inert gas between mould and membrane
EP0028637A1 (en) * 1979-05-21 1981-05-20 Rockwell International Corp Method of fabricating a composite structure.
EP0478033A1 (en) * 1990-08-30 1992-04-01 Dsm N.V. Process for making honeycomb sandwich panels
EP1136238A3 (en) * 2000-03-17 2003-10-15 DLR Deutsches Zentrum für Luft- und Raumfahrt e.V. Method and apparatus for manufacturing a workpiece from fibre reinforced material
US6818159B2 (en) 2000-03-17 2004-11-16 Deutsches Zentrum Fuer Luft-Und Raumfahrt E.V. Process for the production of a composite consisting of a fiber reinforced material
CN102285125A (en) * 2010-04-23 2011-12-21 空中巴士运作公司 Process for manufacturing a piece that is made of composite material and device for its implementation

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0028637A1 (en) * 1979-05-21 1981-05-20 Rockwell International Corp Method of fabricating a composite structure.
EP0028637A4 (en) * 1979-05-21 1983-02-09 Rockwell International Corp Method of fabricating a composite structure.
FR2459118A1 (en) * 1979-06-18 1981-01-09 Poudres & Explosifs Ste Nale Moulding of fibre reinforced thermosetting prepregs - in heated autoclave, under flexible membrane, whilst passing inert gas between mould and membrane
EP0478033A1 (en) * 1990-08-30 1992-04-01 Dsm N.V. Process for making honeycomb sandwich panels
EP1136238A3 (en) * 2000-03-17 2003-10-15 DLR Deutsches Zentrum für Luft- und Raumfahrt e.V. Method and apparatus for manufacturing a workpiece from fibre reinforced material
US6818159B2 (en) 2000-03-17 2004-11-16 Deutsches Zentrum Fuer Luft-Und Raumfahrt E.V. Process for the production of a composite consisting of a fiber reinforced material
CN102285125A (en) * 2010-04-23 2011-12-21 空中巴士运作公司 Process for manufacturing a piece that is made of composite material and device for its implementation
CN102285125B (en) * 2010-04-23 2016-05-11 空中巴士运作公司 A kind of manufacture method of composite material component and device for carrying out said thereof

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Legal Events

Date Code Title Description
PS Patent sealed
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee