US4624820A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Molding of composite materials
Assignee: Rolls Royce PLC
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Filing: 1985-05-02
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Granted: 1986-11-25
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Expires: 2005-05-02
Abstract
Abstract A method of molding a composite material comprising reinforcing fibres enclosed in a resin matrix. Layers of the resin impregnated fibres are laid-up in a suitably shaped die whereupon the laid-up layers are overlaid by a silicone rubber member which generally corresponds in shape with the die. Hydraulic pressure is exerted upon the silicone rubber member so that it urges the laid-up fibres into the configuration of the die. The whole molding apparatus is placed in an oven and its temperature is raised to that at which consolidation of the laid-up fibres occurs and the resin cures. The exerted hydraulic pressure is progressively reduced during heating as the silicone rubber member thermally expands so as to ensure that the pressure exerted by the silicone rubber member upon the laid-up fibres remains substantially constant.
Inventors
- 👤 David J. Barraclough
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 01:14
CPC Classifications
B; B29; B29C; B29C43/00; B29C43/32; B29C43/58; B29C70/00; B29C70/04; B29C70/28; B29C70/40; B29C70/42; B29C70/44; B29C43/02; B29C43/10; B29C43/12; B29C70/30; B29C70/34
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
165 words
A method of molding a composite material comprising laying up a plurality of layers of resin impregnated fibres in a suitable shaped die, overlaying said resin impregnated fibres with a resilient deformable member generally corresponding in shape with that of said die, preheating the assembly at a temperature below that at which the resin cures, exerting pressure upon said resilient deformable member so that it deforms to urge said laid-up resin impregnated fibres into the configuration of said die, heating the assembly so that said resilient deformable member thermally expands to increase the pressure exerted thereby upon said resin impregnated laid-up fibres whilst simultaneously decreasing the pressure exerted upon said resilient deformable member at such a rate that the pressure exerted by said resilient deformable member upon said resin impregnated laid-up fibres remains substantially constant and continuing the heating of said resin impregnated fibres and the maintenance of the exertion of said substantially constant pressure thereon until said laid-up resin impregnated fibres have been consolidated.
Claim 2
Independent Claim
165 words
A method of molding a composite material comprising laying up a plurality of layers of resin impregnated fibres in a suitable shaped die, overlaying said resin impregnated fibres with a resilient deformable member generally corresponding in shape with that of said die, preheating the assembly at a temperature below that at which the resin cures, exerting pressure upon said resilient deformable member so that it deforms to urge said laid-up resin impregnated fibres into the configuration of said die, heating the assembly so that said resilient deformable member thermally expands to increase the pressure exerted thereby upon said resin impregnated laid-up fibres whilst simultaneously decreasing the pressure exerted upon said resilient deformable member at such a rate that the pressure exerted by said resilient deformable member upon said resin impregnated laid-up fibres remains substantially constant and continuing the heating of said resin impregnated fibres and the maintenance of the exertion of said substantially constant pressure thereon until said laid-up resin impregnated fibres have been consolidated.
Claim 3
Dependent Claim
51 words
A method of molding a composite material as claimed in claim 1 wherein said fibres are impregnated with a thermosetting resin and the heating of said resin impregnated fibres and the maintenance of said substantially constant pressure thereon are continued until said fibres have been consolidated and said resin has cured.
Claim 4
Dependent Claim
27 words
A method of molding a composite material as claimed in claim 1 wherein said pressure applied to said resilient deformable member is applied by hydraulically operated means.
Claim 5
Dependent Claim
46 words
A method of molding a composite material as claimed in claim 1 wherein the region between said die and said resilient deformable member which is occupied by said resin impregnated fibres is evacuated prior to the application of heat and pressure to said resin impregnated fibres.
Claim 6
Dependent Claim
23 words
A method of molding a composite material as claimed in claim 1 wherein said resilient deformable member is formed from a silicone rubber.
Claim 7
Dependent Claim
36 words
A method of molding a composite material as claimed in claim 1 wherein said die is so shaped that said composite material is molded into the shape of a nose spinner for a gas turbine engine.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-11-24 | 1990-05-26 | 1990-11-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-11-24 | 1994-05-26 | 1994-11-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-11-24 | 1998-05-26 | 1998-11-25 | $7700.00 | Window Closed / Lapsed |