Wire and power thermal spray gun

Claim 2

A thermal spray gun comprising: nozzle means for generating an annular heating flame; wire means for feeding a wire of heat fusible material axially from the nozzle within the heating flame such that the wire is melted at a tip of the wire by the heating flame; disintegrating means for disintegrating the melted material from the wire tip and propelling the disintegrated material in a spray stream; powder means for feeding a powder stream coaxially between the wire and the heating flame, thereby commingling the powder and the disintegrated material in the spray stream.

Claim 3

A thermal spray gun according to claim 1 further comprising a gas cap extending forwardly from the nozzle means, and the disintegrating means comprises outer gas means for injecting an annular outer flow of pressurized non-combustible gas radially outwardly of the annular heating flame.

Claim 4

A thermal spray gun according to claim 2 further comprising inner gas means for injecting an annular inner flow of pressurized gas from the nozzle means adjacent to the wire.

Claim 5

A thermal spray gun according to claim 2 further comprising intermediate gas means for injecting an annular intermediate flow of pressurized gas from the nozzle means coaxially between the heating flame and the powder stream.

Claim 6

A thermal spray gun according to claim 2 wherein the heating flame is generated by combusting a mixture of a combustion gas and oxygen.

Claim 7

A thermal spray gun for spraying at high velocity to produce a dense and tenacious coating, comprising a nozzle member with a nozzle face, a gas cap extending from the nozzle member and having an inwardly facing cylindrical wall defining a combustion chamber with an axis, an open end and an opposite end bounded by the nozzle face, combustible gas means for injecting an annular flow of a combustible mixture of a combustion gas and oxygen from the nozzle member coaxially into the combustion chamber, outer gas means for injecting an annular outer flow of pressurized noncombustible gas adjacent to the cylindrical wall radially outward of the annular flow of the combustible mixture, wire means for feeding thermal spray wire of heat fusable material axially from the nozzle into the combustion chamber to a point where a wire tip is formed, powder means for feeding powder in a carrier gas annularly from the nozzle member into the combustion chamber coaxially between the combustible mixture and the wire such that, with a combusting combustible mixture, material is melted and disintegrated from the wire tip and a spray stream containing the powder and the heat fusible material commingle in finely divided form is propelled through the open end.

Claim 8

A thermal spray gun for spraying at high velocity to produce a dense and tenacious coating, comprising a nozzle member with a nozzle face, a gas cap extending from the nozzle member and having an inwardly facing cylindrical wall defining a combustion chamber with an axis, an open end and an opposite end bounded by the nozzle face, combustible gas means for injecting an annular flow of a combustible mixture of a combustion gas and oxygen from the nozzle member coaxially into the combustion chamber, outer gas means for injecting an annular outer flow of pressurized noncombustible gas adjacent to the cylindrical wall radially outward of the annular flow of the combustible mixture, wire means for feeding thermal spray wire of heat fusable material axially from the nozzle into the combustion chamber to a point where a wire tip is formed, powder means for feeding powder in a carrier gas annularly from the nozzle member into the combustion chamber coaxially between the combustible mixture and the wire such that, with a combusting combustible mixture, material is melted and disintegrated from the wire tip and a spray stream containing the powder and the heat fusible material commingle in finely divided form is propelled through the open end.

Claim 9

A thermal spray gun according to claim 6 further comprising inner gas means for injecting an annular inner flow of pressurized gas from the nozzle member into the combustion chamber adjacent to the wire.

Claim 10

A thermal spray gun according to claim 6 further comprising intermediate gas means for injecting an annular intermediate flow of pressurized gas from the nozzle member into the combustion chamber coaxially between the combustible mixture and the powder-carrier gas.

Claim 11

A thermal spray gun according to claim 6 wherein the nozzle member comprises a tubular outer portion defining an outer annular orifice means for injecting the annular flow of the combustion mixture into the combustion chamber, and a tubular inner portion having therein an annular inner gas orifice means adjacent the wire for injecting the annular inner flow into the combustion chamber and powder orifice means for feeding the powder-carrier gas into the combustion chamber, and wherein the inner portion protrudes into the combustion chamber forwardly of the outer portion.

Claim 12

A thermal spray gun according to claim 9 wherein a chamber length is defined by a shortest distance from the nozzle face to the open end, and the inner portion protrudes by a distance between about 10% and 40% of the chamber length.

Claim 13

A thermal spray gun according to claim 9 wherein the outer annular orifice means includes an annular opening into the combustion chamber with a radially inward side bounded by an outer wall of the inner portion, the outer wall extending forwardly from the annular opening with a curvature toward the axis.

Claim 14

A thermal spray gun according to claim 11 wherein the curvature is such as to define a generally hemispherical nozzle face on the inner portion.

Claim 15

A thermal spray gun according to claim 9 wherein the outer gas means includes the nozzle member and a rearward portion of the cylindrical wall defining a forwardly converging slot therebetween exiting into the combustion chamber.

Claim 16

A thermal spray gun according to claim 13 wherein the combustion chamber converges forwardly from the nozzle member at an angle with the axis less than a corresponding angle of the converging annular slot.

Claim 17

A thermal spray gun according to claim 6 wherein the combustible gas means is disposed so as to inject the combustible mixture into the combustion chamber from a circular location on the nozzle face, the circular location having a diameter approximately equal to the diameter of the open end.

Claim 18

A thermal spray gun according to claim 15 wherein the open end is spaced axially from the nozzle face by a shortest distance of between approximately one and two times the diameter of the circular location.

Claim 19

A thermal spray gun according to claim 6 wherein the combustible mixture is injected into the combustion chamber at a pressure therein of at least two atmospheres above ambient atmospheric pressure, such that the spray stream is supersonic.

Claim 20

A thermal spray gun according to claim 17 wherein the point where the wire tip is formed is proximate the open end of the combustion chamber.

Claim 23

A method according to claim 19 further comprising injecting an annular inner flow of pressurized gas from the nozzle into the combustion chamber adjacent to the wire.

Claim 24

A method according to claim 19 further comprising injecting an annular intermediate flow of pressurized gas from the nozzle member into the combustion chamber coaxially between the combustible mixture and the powder-carrier gas.

Claim 25

A method according to claim 19 wherein the combustible mixture is injected at a sufficient pressure into the cylindrical chamber to produce at least 8 visible shock diamonds in the spray stream in the absence of thermal spray wire and powder-carrier gas in the combustion chamber.

Claim 26

A method according to claim 19 further comprising selecting the combustion gas from the group consisting of propylene gas and methylacetylene-propadiene gas.

Claim 27

A method according to claim 19 further comprising providing oxygen to the combustible mixture at a flow rate of at least about 80% of the annular outer flow.

Claim 28

A method according to claim 19 wherein the combustible mixture is injected through an annular orifice into the combustion chamber.

Claim 29

A method according to claim 19 wherein the powder is selected from the group consisting of carbides, borides and nitrides of at least one metal, and diamond.

Claim 30

A method according to claim 26 wherein the powder is nonfusible at atmospheric pressure.