GB1260409A - Carbon fibre reinforced resin plastics sheet - Google Patents
Carbon fibre reinforced resin plastics sheetInfo
- Publication number
- GB1260409A GB1260409A GB1244969A GB1244969A GB1260409A GB 1260409 A GB1260409 A GB 1260409A GB 1244969 A GB1244969 A GB 1244969A GB 1244969 A GB1244969 A GB 1244969A GB 1260409 A GB1260409 A GB 1260409A
- Authority
- GB
- United Kingdom
- Prior art keywords
- resin
- carbon fibre
- film
- sheet
- tows
- 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
- 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
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
-
- 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
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/504—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands
-
- 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
- B29C70/82—Forcing wires, nets or the like partially or completely into the surface of an article, e.g. by cutting and pressing
-
- 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
- B29C70/685—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 laminating inserts between two plastic films or plates
- B29C70/687—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 laminating inserts between two plastic films or plates the inserts being oriented, e.g. nets or meshes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/24—Condition, form or state of moulded material or of the material to be shaped crosslinked or vulcanised
- B29K2105/246—Uncured, e.g. green
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2307/00—Use of elements other than metals as reinforcement
-
- 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
- B29L2007/00—Flat articles, e.g. films or sheets
- B29L2007/008—Wide strips, e.g. films, webs
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Reinforced Plastic Materials (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
1,260,409. Laminates. DEFENCE, SECRETARY OF STATE FOR. 10 March, 1970 [10 March, 1969], No. 12449/60. Heading B5N. [Also in Divisions C1 and D1] A sheet of carbon fibre reinforced resin is prepared by laying up tows of carbon fibre in generally parallel array against at least one layer or film of resin matrix material, flattening the resin and carbon fibre together to a desired thickness by the application of a rolling pressure in the general direction of fibre alignment and simultaneously applying heat in the region of the pressure application to soften the resin. The resin film may be laid on a platten or sheet from which it easily parts, the tows of carbon fibre may be aligned on the resin film, a second resin film positioned over the aligned tows and a heated roller under spring-pressure or at a desired distance from the platten passed along the second film in the general direction of the fibres. The second resin film may be substituted by a sheet of parting agent or parting agent treated material. In a preferred embodiment, one side of each of two sheets of paper which have been treated with parting agent are sprayed or otherwise coated with a resin and hardener diluted with a solvent, the solvent is allowed to evaporate and tows of carbon fibre in generally parallel array are laid up on the resin coated side of one of the sheets. The resin treated side of the other sheet is placed on top of the fibre layer to form a laminate, which is flattened and the resin softened by rolling and heating. Elimination of the solvent may be encouraged by heating, e.g. in an oven, at a temperature below the curing temperature of the resin. The sheets of paper may then be removed from the laminate. The resin used may be an epoxy resin, a polyester resin, a polyimide, a phenolic or a Friedel Crafts type resin, a preferred resin coating being 50% by wt. epoxy resin, with acetone solvent and an additional 4% of hardener. At least one pair of rollers may be used to apply the rolling pressure. A laminated article may be produced by laying several of the sheets so produced upon one another, e.g. on a mandrel or in a mould, and curing the resin content by application of heat.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1244969A GB1260409A (en) | 1969-03-10 | 1969-03-10 | Carbon fibre reinforced resin plastics sheet |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1244969A GB1260409A (en) | 1969-03-10 | 1969-03-10 | Carbon fibre reinforced resin plastics sheet |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1260409A true GB1260409A (en) | 1972-01-19 |
Family
ID=10004807
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1244969A Expired GB1260409A (en) | 1969-03-10 | 1969-03-10 | Carbon fibre reinforced resin plastics sheet |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1260409A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5580531A (en) * | 1978-12-14 | 1980-06-17 | Toho Beslon Co | Carbon fiber prepreg and method |
JPS5582112A (en) * | 1978-12-19 | 1980-06-20 | Toray Ind Inc | Resin composition for fiber-reinforcing |
JPS5823830A (en) * | 1982-01-16 | 1983-02-12 | Toho Rayon Co Ltd | Preparation of prepreg |
FR2561578A1 (en) * | 1984-03-23 | 1985-09-27 | Tarkett Ab | PROCESS FOR MANUFACTURING REINFORCED PLASTIC STRIPS OR SHEETS AND STRIPS OR SHEETS PRODUCED ACCORDING TO THIS PROCESS |
FR2645069A1 (en) * | 1989-03-31 | 1990-10-05 | Onera (Off Nat Aerospatiale) | PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL CONSISTING OF A THERMOPLASTIC MATRIX REINFORCED WITH LONG FIBERS AND COMPOSITE MATERIAL OBTAINED BY THIS PROCESS |
EP0535214A1 (en) * | 1991-04-04 | 1993-04-07 | LINCOLN, James D. | Unidirectional carbon/phenolic prepreg material and method of manufacture |
CN116200687A (en) * | 2023-02-23 | 2023-06-02 | 集美大学 | Transverse fiber reinforced armored aluminum alloy and preparation method thereof |
-
1969
- 1969-03-10 GB GB1244969A patent/GB1260409A/en not_active Expired
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5580531A (en) * | 1978-12-14 | 1980-06-17 | Toho Beslon Co | Carbon fiber prepreg and method |
JPS6234775B2 (en) * | 1978-12-14 | 1987-07-29 | Toho Rayon Kk | |
JPS6131739B2 (en) * | 1978-12-19 | 1986-07-22 | Toray Industries | |
JPS5582112A (en) * | 1978-12-19 | 1980-06-20 | Toray Ind Inc | Resin composition for fiber-reinforcing |
JPS5823830A (en) * | 1982-01-16 | 1983-02-12 | Toho Rayon Co Ltd | Preparation of prepreg |
JPS6047290B2 (en) * | 1982-01-16 | 1985-10-21 | 東邦レーヨン株式会社 | Prepreg manufacturing method |
FR2561578A1 (en) * | 1984-03-23 | 1985-09-27 | Tarkett Ab | PROCESS FOR MANUFACTURING REINFORCED PLASTIC STRIPS OR SHEETS AND STRIPS OR SHEETS PRODUCED ACCORDING TO THIS PROCESS |
GB2156396A (en) * | 1984-03-23 | 1985-10-09 | Tarkett Ab | Filament reinforced plastics sheets |
FR2645069A1 (en) * | 1989-03-31 | 1990-10-05 | Onera (Off Nat Aerospatiale) | PROCESS FOR MANUFACTURING A COMPOSITE MATERIAL CONSISTING OF A THERMOPLASTIC MATRIX REINFORCED WITH LONG FIBERS AND COMPOSITE MATERIAL OBTAINED BY THIS PROCESS |
EP0394081A2 (en) * | 1989-03-31 | 1990-10-24 | Office National D'etudes Et De Recherches Aerospatiales | Method for producing a composite comprising a thermoplastic matrix reinforced with long fibres, and composite obtained by this method |
EP0394081A3 (en) * | 1989-03-31 | 1991-01-16 | Office National D'etudes Et De Recherches Aerospatiales | Method for producing a composite comprising a thermoplastic matrix reinforced with long fibres, and composite obtained by this method |
EP0535214A1 (en) * | 1991-04-04 | 1993-04-07 | LINCOLN, James D. | Unidirectional carbon/phenolic prepreg material and method of manufacture |
EP0535214A4 (en) * | 1991-04-04 | 1993-09-08 | James D. Lincoln | Unidirectional carbon/phenolic prepreg material and method of manufacture |
CN116200687A (en) * | 2023-02-23 | 2023-06-02 | 集美大学 | Transverse fiber reinforced armored aluminum alloy and preparation method thereof |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |