GB1441919A - Production of fibre reinforced synthetic resin articles - Google Patents
Production of fibre reinforced synthetic resin articlesInfo
- 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
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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
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.
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)
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 |
-
1972
- 1972-07-26 GB GB3502672A patent/GB1441919A/en not_active Expired
Cited By (8)
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 |