Claims
- 1. A method for reinforcing a part having a complex surface, comprising the steps of:
- providing an uncured supported elastomer material comprising a fibrous reinforcement material and a layer of uncured elastomer material supported on and infused into said fibrous reinforcement material so as to provide an uncured supported elastomer material between and encompassing said fibrous reinforcement material thereby providing an effective intimate contact between the fibrous reinforcement material and the uncured elastomeric material supported thereon;
- providing a part having a complex surface to be reinforced;
- applying said uncured supported elastomer material to said complex surface; and
- curing said uncured supported elastomer material.
- 2. A method according to claim 1, wherein said step of providing said uncured supported elastomer material comprises the steps of:
- providing a fibrous reinforcement material;
- providing a sheet of uncured elastomer material substantially adjacent to said fibrous reinforcement material;
- exposing said layer and said fibrous reinforcement to a temperature below a curing temperature and above a flow point of said uncured elastomer material, and a pressure sufficient that said uncured elastomer material flows into said fibrous reinforcement material, so as to provide said uncured supported elastomer material.
- 3. A method according to claim 1, wherein said applying step comprises the step of adhesively applying said uncured supported elastomer material to said complex surface using a method selected from the group consisting of resin transfer molding, compression molding, bonding, autoclave bonding and combinations thereof.
- 4. A method according to claim 1, wherein said part is a helicopter rotor having a complex surface.
- 5. A method according to claim 1, wherein said part is a propeller having a complex surface.
- 6. A method according to claim 1, wherein said part is a gas turbine engine fan blade having a complex surface.
- 7. A method according to claim 1, wherein said part is a nacelle gas path component having a complex surface.
- 8. A method according to claim 1, wherein said part is a compressor airfoil having a complex surface.
- 9. A method according to claim 1, wherein said part is a gas path vane having a complex surface.
- 10. A method according to claim 1, wherein said part is a strut having a complex surface.
Parent Case Info
This is a Division of application Ser. No. 08/645,669, filed May 14, 1996, now U.S. Pat. No. 5,786,285.
US Referenced Citations (6)
Divisions (1)
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Number |
Date |
Country |
Parent |
645669 |
May 1996 |
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