Claims
- 1. In a thermal spray method comprising the steps of:
- continuously combusting a fuel and oxidant under pressure within a restricting volume of a combustion chamber and expanding the products o combustion of said fuel and oxidant as gas into an extended nozzle having a throat opening to said combustion chamber and producing at least a sonic flow stream of gases from an said extended nozzle to produce and direct a supersonic jet of said gases toward a workpiece surface to be coated;
- feeding a powdered material to said stream to be heated b said stream and projected onto the workpiece surface;
- the improvement wherein the step of feeding said powdered material comprises feeding said powdered material into said extended nozzle at a point downstream from said throat and after expansion of the gases to a temperature which limits the heating of said powdered material to that which raises the temperature of particles of said powdered material to that lower than the melting point of said powdered material, and wherein said method further comprises maintaining an in-transit temperature of said particles from said feeding point to said workpiece below said melting point, and providing a sufficient velocity to said particles such that impact energy caused by said particles striking said workpiece is transformed into heat, thereby increasing the temperature of the particles to the fusion temperature of the particles, thereby fusing the powdered material to form a dense coating on the workpiece surface.
- 2. The method of claim 1, wherein the step of feeding said powdered material to said stream comprises feeding said powder into the stream at a point along the stream where an expansion of said gases has reduced the temperature of said stream to less than the temperature of the melting point of said material being sprayed.
- 3. The method of claim 1, wherein the oxidant is air.
- 4. The method of claim 1, wherein the oxidant is a mixture of air and pure oxygen.
- 5. The method of claim 1, wherein the oxidant is pure oxygen.
- 6. The method of claim 1, wherein the fuel and oxidant are combusted at combustion pressures such that the temperature of solid particles of the powdered material striking said workpiece is minimized to achieve impact energy values sufficient to cause fusion of the particles to form a coating.
- 7. The method of claim 6, wherein combustion is effected at a pressure greater than 250 psig.
- 8. The method of claim 6, wherein combustion is effected at a pressure greater than 500 psig.
- 9. The method of clam 6, wherein combustion is effected at a pressure greater than 1,000 psig.
- 10. The method of claim 1, wherein the heating of said powder particles to below the melting point thereof is effected by using a first temperature jet and said method further comprises accelerating the heated solid particles toward the workpiece using a second jet.
- 11. The method of claim 1, wherein the powder to be sprayed is a mixture of at least two materials of different melting points, and where, upon impact, the material of lower melting point is fused, while the material of higher melting point remains in the solid state throughout the method.
- 12. The method of claim 1, wherein the powder to be sprayed is a mixture of tungsten carbide and cobalt and where only cobalt is fused upon impact.
Parent Case Info
This application is a continuation-in-part of application Ser. No. 07/641,958, filed Jan. 16, 1991, now U.S. Pat. No. 5,120,582, and entitled "MAXIMUM COMBUSTION ENERGY CONVERSION AIR FUEL INTERNAL BURNER".
US Referenced Citations (12)
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
641958 |
Jan 1991 |
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