Claims
- 1. A method for forming a metal matrix composite material, wherein the composite is formed from woven or chopped graphite, the method including the steps of:impregnating the graphite with a polymer containing a metal powder; drying the graphite; passing the graphite through a molten bath of metal alloy that is at a temperature to carburise the polymer and so form the composite material; and exerting pressure on the composite material to remove excess metal alloy therefrom.
- 2. The method of claim 1 wherein the composite is formed from woven or chopped graphite and a ceramic material.
- 3. The method of claim 1 wherein the woven graphite is of the type 3K TOW, 380 g/m2, M60/T300.
- 4. The method of claim 1 wherein the polymer comprises either a polymer solution or molten polymer .
- 5. The method of claim 1 wherein the metal powder is formed from a metal alloy.
- 6. The method of claim 5 wherein the metal alloy constitutes at least 20% w/w of the polymer.
- 7. The method of claim 6 wherein the metal powder is formed from an alloy including one of aluminum, nickel and molybdenum.
- 8. The method of claim 1 wherein the step of drying the graphite comprises passing the graphite through an electric furnace.
- 9. The method of claim 1 wherein the molten metal alloy is formed from an alloy including one of aluminum, nickel and molybdenum.
- 10. The method of claim 1 wherein the step of exerting pressure on the composite material comprises passing the composite through a set of rollers that are capable of exerting about 35 to 40 tons of compression and which squeeze out substantially all excess metal alloy from the composite material.
- 11. The method of claim 1 wherein a metal is applied to the composite material to provide bonding of said woven or chopped graphite to said metal powder.
- 12. The method of claim 11 wherein the metal is titanium, beryllium or a metal alloy.
- 13. The method of claim 12 wherein the metal is applied by plasma spraying or hot sheet pressing.
- 14. A method for forming a metal matrix composite material, wherein the composite is formed from woven or chopped graphite, the method including the steps of:impregnating the graphite with a molten polymer containing an alloy powder; passing the graphite through a molten bath of metal alloy that is at a temperature to carburise the polymer and so form the composite material; drying the impregnated graphite; and rolling the impregnated graphite in a set of rollers to form a rolled composite material.
- 15. The method of claim 14 wherein the composite is formed from woven or chopped graphite and a ceramic material.
- 16. The method of claims 14 wherein the woven graphite is of the type 3K TOW, 380 g/m2, M60/T300.
- 17. The method of claim 14 wherein the high temperature alloy is a titanium or nickel alloy.
- 18. The method of claim 17 wherein the metal alloy constitutes up to about 50% w/w of the polymer.
- 19. The method of claim 14 wherein the step of drying the graphite comprises passing the graphite through an electric furnace.
- 20. The method of claim 14 wherein the step of exerting pressure on the impregnated graphite comprises passing the graphite through a set of rollers that are capable of exerting about 35 to 40 tons of compression.
Priority Claims (1)
Number |
Date |
Country |
Kind |
9804838 |
Dec 1998 |
SG |
|
Parent Case Info
This is a divisional of co-pending U.S. application Ser. No. 09/470,522 filed on Dec. 22, 1999.
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