GB835822A - Improvements in or relating to moulds, jigs and like structures - Google Patents
Improvements in or relating to moulds, jigs and like structuresInfo
- Publication number
- GB835822A GB835822A GB3246857A GB3246857A GB835822A GB 835822 A GB835822 A GB 835822A GB 3246857 A GB3246857 A GB 3246857A GB 3246857 A GB3246857 A GB 3246857A GB 835822 A GB835822 A GB 835822A
- Authority
- GB
- United Kingdom
- Prior art keywords
- surface coat
- fibrous material
- resin
- synthetic resin
- lightweight filler
- 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
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J9/00—Working-up of macromolecular substances to porous or cellular articles or materials; After-treatment thereof
- C08J9/32—Working-up of macromolecular substances to porous or cellular articles or materials; After-treatment thereof from compositions containing microballoons, e.g. syntactic foams
-
- 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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
- B29C33/3842—Manufacturing moulds, e.g. shaping the mould surface by machining
- B29C33/3857—Manufacturing moulds, e.g. shaping the mould surface by machining by making impressions of one or more parts of models, e.g. shaped articles and including possible subsequent assembly of the parts
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Health & Medical Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Laminated Bodies (AREA)
Abstract
Moulds, jigs, and like structures are made by applying to the surface of a pattern in the following sequence: (i) a synthetic resin surface coat, particularly one which may be hardened at room temperature, e.g. an unsaturated polyester or an epoxide resin; (ii) a woven or mat sheet of a fibrous material, e.g. glass fibres; and (iii) a mixture of a lightweight filler and a synthetic resin binding agent, e.g. an epoxide or polyester resin as in (i) and allowing the synthetic resin in the composite article to harden. The surface coat usually contains a mineral filler, e.g. slate dust, and a thixotropic agent, e.g. silica aerogel. The lightweight filler may consist of hollow particles formed from synthetic resinous materials, e.g. phenol-formaldehyde or polystyrene resin or naturallyoccurring materials which have been heat-treated to reduce their bulk density to less than 20 lb/cu. ft., e.g. perlite or vermiculite. It is customary to allow the surface coat to gel in which case a second surface coat and/or a layer of adhesive is applied before covering with the fibrous material which is preferably glass-fibre. If greater strength is needed a further layer of fibrous material may be applied after the mixture containing the lightweight filler.ALSO:Moulds, jigs, and like structures are made by applying to the surface of a pattern in the following sequence (i) a synthetic resin surface coat, particularly one which may be hardened at room temperature, e.g. an unsaturated polyester or an epoxide resin (ii) a woven or mat sheet of a fibrous material, and (iii) a mixture of a lightweight filler and a synthetic resin binding agent, e.g. an epoxide or polyester resin as in (i) and allowing the synthetic resin in the composite article to harden. The surface coat usually contains a mineral filler, e.g. slate dust, and a thixotropic agent, e.g. silica aerogel. The lightweight filler may consist of hollow particles formed from synthetic resinous materials, e.g. phenol-formaldehyde or polystyrene resin or naturally-occurring materials which have been heat-treated to reduce their bulk density to less than 20 lb./cu. ft., e.g. perlite or vermiculite. It is customary to allow the surface coat to gel in which case a second surface coat and/or a layer of adhesive is applied before covering with the fibrous material which is preferably glass-fibre. If greater strength is needed a further layer of fibrous material may be applied after the mixture containing the lightweight filler.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3246857A GB835822A (en) | 1957-10-17 | 1957-10-17 | Improvements in or relating to moulds, jigs and like structures |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3246857A GB835822A (en) | 1957-10-17 | 1957-10-17 | Improvements in or relating to moulds, jigs and like structures |
Publications (1)
Publication Number | Publication Date |
---|---|
GB835822A true GB835822A (en) | 1960-05-25 |
Family
ID=10339043
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3246857A Expired GB835822A (en) | 1957-10-17 | 1957-10-17 | Improvements in or relating to moulds, jigs and like structures |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB835822A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2254819A (en) * | 1991-04-16 | 1992-10-21 | British Aerospace | Tooling for the manufacture of composite articles |
CN111958886A (en) * | 2020-07-15 | 2020-11-20 | 天津爱思达航天科技有限公司 | Universal carbon foam composite material die with high yield and preparation method thereof |
CN111958887A (en) * | 2020-07-15 | 2020-11-20 | 天津爱思达航天科技有限公司 | High-precision high-yield carbon foam composite material mold and preparation method |
-
1957
- 1957-10-17 GB GB3246857A patent/GB835822A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2254819A (en) * | 1991-04-16 | 1992-10-21 | British Aerospace | Tooling for the manufacture of composite articles |
GB2254819B (en) * | 1991-04-16 | 1995-07-26 | British Aerospace | Tooling for the manufacture of composite articles |
CN111958886A (en) * | 2020-07-15 | 2020-11-20 | 天津爱思达航天科技有限公司 | Universal carbon foam composite material die with high yield and preparation method thereof |
CN111958887A (en) * | 2020-07-15 | 2020-11-20 | 天津爱思达航天科技有限公司 | High-precision high-yield carbon foam composite material mold and preparation method |
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