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US3914573A Expired / Lapsed US ⏱️ 0.0 years remaining

Coating heat softened particles by projection in a plasma stream of Mach 1 to Mach 3 velocity

Assignee: Geotel Inc
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Filing: 1973-08-06
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Granted: 1975-10-21
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Expires: 1993-08-06
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Abstract

Abstract An electric arc plasma spray gun provides optimum coating of substrates by projecting a stream of plasma at a velocity at or about Mach two, at ambient pressure, and entraining therein particles of material to be coated upon said substrate. Power, pressures and temperatures are employed together with a unique set of interchangeable supersonic nozzles to achieve particle exit velocities of from one to ten thousand feet per second, heating said particles to a temperature below their melting point but sufficient to soften the particles for enhanced coating. Unique parameters of particle size, particle injection angle and particle injection positions are identified for different materials to be entrained in the supersonic plasma stream.

Inventors

  • 👤 Erich Muehlberger

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 21:10
CPC Classifications
B; B05; B05B; B05B7/00; B05B7/16; B05B7/22; B05B7/222; B05B7/226; C; C23; C23C; C23C24/00; C23C24/02; C23C24/04; H; H05; H05H; H05H1/00; H05H1/24; H05H1/26; H05H1/32; H05H1/42

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 177 words
The method of projecting high velocity particles onto a substrate to coat the same, comprising the steps of: establishing a plasma stream, expanding said plasma stream from the throat to the exit of a supersonic nozzle having a ratio of exit area to throat area sufficient to achieve a plasma stream exit velocity greater than Mach 1 and less than Mach 3, injecting into said plasma stream a stream of particles to be projected, said particles having a diameter not greater than about 44 microns, heating said particles to a temperature near but less than their melting point, said last-mentioned step comprising controlling the time of dwell of said particles within said plasma stream by selectively controlling both the angle and position of injection of said particles into said stream substantially at the throat of said nozzle, whereby said particles will be softened, but not melted, and will obtain a velocity that is substantially maximized with respect to the velocity of said plasma stream, and impinging said softened particles against a substrate to thereby coat said substrate.
Claim 2
Independent Claim 177 words
The method of projecting high velocity particles onto a substrate to coat the same, comprising the steps of: establishing a plasma stream, expanding said plasma stream from the throat to the exit of a supersonic nozzle having a ratio of exit area to throat area sufficient to achieve a plasma stream exit velocity greater than Mach 1 and less than Mach 3, injecting into said plasma stream a stream of particles to be projected, said particles having a diameter not greater than about 44 microns, heating said particles to a temperature near but less than their melting point, said last-mentioned step comprising controlling the time of dwell of said particles within said plasma stream by selectively controlling both the angle and position of injection of said particles into said stream substantially at the throat of said nozzle, whereby said particles will be softened, but not melted, and will obtain a velocity that is substantially maximized with respect to the velocity of said plasma stream, and impinging said softened particles against a substrate to thereby coat said substrate.
Claim 3
Dependent Claim 486 words
A supersonic plasma spray gun for projecting particles of high velocity comprising: means for producing a plasma arc at a pre-selected pressure and electrical power, and including nozzle means for expanding plasma produced in said arc to provide a plasma stream having an exit velocity of greater than Mach 1 and less than Mach 3, means for injecting a stream of particles of a size not greater than 44 microns into said plasma stream to be entrained thereby, and means for controlling time of dwell of said particles within said plasma stream so as to heat the particles to a temperature near to, but below, their melting point and to achieve substantially maximized velocity of said particles, said means for controlling dwell time comprising a plurality of nozzles, each including means for selective and alternative attachment to said spray gun, and each having a bore having a ratio of exit area to throat area sufficient to produce the above-mentioned plasma stream exit velocity, and each of said nozzles having a particle injection conduit providing communication between a source of particles exterior to said nozzles and the bore of said nozzle at a point thereof between said exit and throat for injection of said particles into the plasma stream, a first one of said nozzles for use with particles of low melting points such as bronze, copper and aluminum, having its particle injection conduit extending at a large angle (between 25* and 49*) with respect to a normal to the direction of flow of said plasma stream, and communicating with the bore of said nozzle at a point closely adjacent the nozzle exit to thereby provide a short dwell time that prevents premature melting and plating of the nozzle bore, a second one of said nozzles for use with materials of intermediate melting points (2000*F to 3000*F), such as stainless steel, nickel, chromium, and hard facing alloys having its particle injection conduit extending at an intermediate angle (between 7.5* and 25*) with respect to a normal to the direction of plasma stream flow and communicating with the bore of its associated nozzle at a point substantially midway between the throat and exit, but somewhat closer to the throat whereby the dwell time of such intermediate temperature melting point particles is greater than the dwell time achieved by lower temperature particles in said first-mentioned nozzle, and a third one of said nozzles for use with high temperature melting point particles such as tungsten carbide-cobalt, chromium carbide nickel chromium blends, tungsten and molybdenum, having its particle injection conduit extending at a considerably smaller angle (between -13* and 7.5*) with respect to a normal to the direction of the plasma stream and communicating with the bore of its associated nozzle at a point thereof substantially at its throat whereby dwell time of such high temperature particles is at least sufficient to ensure substantial heat softening of the particles without melting.
Claim 4
Dependent Claim 486 words
A supersonic plasma spray gun for projecting particles of high velocity comprising: means for producing a plasma arc at a pre-selected pressure and electrical power, and including nozzle means for expanding plasma produced in said arc to provide a plasma stream having an exit velocity of greater than Mach 1 and less than Mach 3, means for injecting a stream of particles of a size not greater than 44 microns into said plasma stream to be entrained thereby, and means for controlling time of dwell of said particles within said plasma stream so as to heat the particles to a temperature near to, but below, their melting point and to achieve substantially maximized velocity of said particles, said means for controlling dwell time comprising a plurality of nozzles, each including means for selective and alternative attachment to said spray gun, and each having a bore having a ratio of exit area to throat area sufficient to produce the above-mentioned plasma stream exit velocity, and each of said nozzles having a particle injection conduit providing communication between a source of particles exterior to said nozzles and the bore of said nozzle at a point thereof between said exit and throat for injection of said particles into the plasma stream, a first one of said nozzles for use with particles of low melting points such as bronze, copper and aluminum, having its particle injection conduit extending at a large angle (between 25* and 49*) with respect to a normal to the direction of flow of said plasma stream, and communicating with the bore of said nozzle at a point closely adjacent the nozzle exit to thereby provide a short dwell time that prevents premature melting and plating of the nozzle bore, a second one of said nozzles for use with materials of intermediate melting points (2000*F to 3000*F), such as stainless steel, nickel, chromium, and hard facing alloys having its particle injection conduit extending at an intermediate angle (between 7.5* and 25*) with respect to a normal to the direction of plasma stream flow and communicating with the bore of its associated nozzle at a point substantially midway between the throat and exit, but somewhat closer to the throat whereby the dwell time of such intermediate temperature melting point particles is greater than the dwell time achieved by lower temperature particles in said first-mentioned nozzle, and a third one of said nozzles for use with high temperature melting point particles such as tungsten carbide-cobalt, chromium carbide nickel chromium blends, tungsten and molybdenum, having its particle injection conduit extending at a considerably smaller angle (between -13* and 7.5*) with respect to a normal to the direction of the plasma stream and communicating with the bore of its associated nozzle at a point thereof substantially at its throat whereby dwell time of such high temperature particles is at least sufficient to ensure substantial heat softening of the particles without melting.
Claim 5
Independent Claim 295 words
A method of projecting particles to be spray-coated upon a substrate wherein the particles are borne by a supersonic stream of plasma having a velocity greater than Mach 1 and less than Mach 3 and wherein the velocity of the particles is substantially maximized as the particles are heated, said method comprising: providing an electrical plasma jet torch having a gas vortex chamber communicating with a nozzle passage having a throat, said torch also having a rear electrode extending adjacent said nozzle passage, creating and maintaining an electric arc in said nozzle passage between said rear electrode and a forward electrode that defines said nozzle passage, introducing plasma arc gas into said vortex chamber in a direction that is substantially tangential thereto but inclined forwardly through a relatively small angle and causing said gas to flow vortically and helically in said vortex chamber and toward said nozzle passage, ionizing said plasma arc gas in said electric arc, constricting said ionized gas as it flows from said rear electrode toward the throat of said nozzle passage, and continuously expanding said ionized gas as it flows from said throat to the exit of said nozzle passage to attain said supersonic velocity, injecting into said nozzle, through the boundary layer of said ionized gas, a stream of particles having a size not greater than 44 microns and having melting temperatures above 3000*F, said last-mentioned step including injecting said particles into said nozzle at an angle within the range of -13* and 7.5* relative to said plasma flow and at a position within said nozzle between 0.032 and 0.142 inches downstream of the nozzle throat, so that the particles are heated to a temperature near but less than their melting point, and projecting said heated particles against a substrate.
Claim 6
Independent Claim 295 words
A method of projecting particles to be spray-coated upon a substrate wherein the particles are borne by a supersonic stream of plasma having a velocity greater than Mach 1 and less than Mach 3 and wherein the velocity of the particles is substantially maximized as the particles are heated, said method comprising: providing an electrical plasma jet torch having a gas vortex chamber communicating with a nozzle passage having a throat, said torch also having a rear electrode extending adjacent said nozzle passage, creating and maintaining an electric arc in said nozzle passage between said rear electrode and a forward electrode that defines said nozzle passage, introducing plasma arc gas into said vortex chamber in a direction that is substantially tangential thereto but inclined forwardly through a relatively small angle and causing said gas to flow vortically and helically in said vortex chamber and toward said nozzle passage, ionizing said plasma arc gas in said electric arc, constricting said ionized gas as it flows from said rear electrode toward the throat of said nozzle passage, and continuously expanding said ionized gas as it flows from said throat to the exit of said nozzle passage to attain said supersonic velocity, injecting into said nozzle, through the boundary layer of said ionized gas, a stream of particles having a size not greater than 44 microns and having melting temperatures above 3000*F, said last-mentioned step including injecting said particles into said nozzle at an angle within the range of -13* and 7.5* relative to said plasma flow and at a position within said nozzle between 0.032 and 0.142 inches downstream of the nozzle throat, so that the particles are heated to a temperature near but less than their melting point, and projecting said heated particles against a substrate.
Claim 7
Independent Claim 179 words
The method of high velocity spraying of particles comprising the steps of: generating a stream of plasma, flowing said plasma stream through a converging diverging supersonic nozzle having a throat and an exit, causing said plasma stream to expand from the nozzle throat to the nozzle exit to provide a plasma stream exit velociTy of between Mach 1 and Mach 3 at ambient exit pressure, and also causing the plasma stream to decrease in density from a high density at said throat to a lower density at said exit, feeding to said nozzle a flow of particles having a maximum dimension of 44 microns, injecting said particles through the boundary layer and toward the center of said plasma stream at a point within said nozzle where said plasma stream has substantially said high density so as to heat said particles to a temperature near but less than the melting point thereof, whereby greater kinetic energy is transferred from said plasma stream to the particles injected therein, and impinging said heated particles against a substrate to thereby coat said substrate.
Claim 8
Independent Claim 179 words
The method of high velocity spraying of particles comprising the steps of: generating a stream of plasma, flowing said plasma stream through a converging diverging supersonic nozzle having a throat and an exit, causing said plasma stream to expand from the nozzle throat to the nozzle exit to provide a plasma stream exit velociTy of between Mach 1 and Mach 3 at ambient exit pressure, and also causing the plasma stream to decrease in density from a high density at said throat to a lower density at said exit, feeding to said nozzle a flow of particles having a maximum dimension of 44 microns, injecting said particles through the boundary layer and toward the center of said plasma stream at a point within said nozzle where said plasma stream has substantially said high density so as to heat said particles to a temperature near but less than the melting point thereof, whereby greater kinetic energy is transferred from said plasma stream to the particles injected therein, and impinging said heated particles against a substrate to thereby coat said substrate.
Claim 9
Dependent Claim 56 words
The method of claim 4, wherein said step of injecting particles into said plasma stream comprises injecting said particles into said nozzle in a direction that is inclined rearwardly with respect to the direction of flow of said plasma stream whereby transfer of kinetic energy from said plasma stream to said particles is still further increased.
Claim 10
Dependent Claim 328 words
Particle spraying apparatus for generating and projecting a stream of plasma exiting therefrom at a Mach number exit velocity greater than 1 and less than 3, said apparatus comprising: a gun having front and back electrodes and a vortex chamber extending about said back electrode, means for feeding gas under pressure into said vortex chamber adjacent said back electrode, means for energizing said electrodes to form an arc therebetween to ionize said gas and create a plasma stream flowing to and through said front electrode, said front electrode comprising an exit nozzle communicating with said vortex chamber and having an exit, having a throat spaced downstream of said back electrode, and having a portion diverging from said throat to the exit of said nozzle to provide a ratio of area of said exit to area of said throat sufficient to provide an exit velocity greater than Mach 1 and less than Mach 3, said nozzle having an axis along which said plasma stream flows, said means for feeding gas under pressure including means for effecting a pressure in said vortex chamber in the vicinity of said arc having a relation to ambient pressure sufficient to provide said Mach number exit velocity with said ratio of areas, and means for entraining and heating in said plasma stream a flow of particles having a size of less than 44 microns to be coated upon a substrate against which said plasma stream impinges, said means for entraining and heating causing said particles to be heated to a temperature near but below their melting point, said means for entraining comprising a particle injection conduit intersecting the nozzle at a point adjacent the nozzle throat wherein said plasma stream is of relatively higher density, and means for feeding said particles through said conduit and through the boundary layer of said plasma stream toward the center thereof whereby both transferred kinetic energy and dwell time of the particles in the plasma stream are increased.
Claim 11
Dependent Claim 328 words
Particle spraying apparatus for generating and projecting a stream of plasma exiting therefrom at a Mach number exit velocity greater than 1 and less than 3, said apparatus comprising: a gun having front and back electrodes and a vortex chamber extending about said back electrode, means for feeding gas under pressure into said vortex chamber adjacent said back electrode, means for energizing said electrodes to form an arc therebetween to ionize said gas and create a plasma stream flowing to and through said front electrode, said front electrode comprising an exit nozzle communicating with said vortex chamber and having an exit, having a throat spaced downstream of said back electrode, and having a portion diverging from said throat to the exit of said nozzle to provide a ratio of area of said exit to area of said throat sufficient to provide an exit velocity greater than Mach 1 and less than Mach 3, said nozzle having an axis along which said plasma stream flows, said means for feeding gas under pressure including means for effecting a pressure in said vortex chamber in the vicinity of said arc having a relation to ambient pressure sufficient to provide said Mach number exit velocity with said ratio of areas, and means for entraining and heating in said plasma stream a flow of particles having a size of less than 44 microns to be coated upon a substrate against which said plasma stream impinges, said means for entraining and heating causing said particles to be heated to a temperature near but below their melting point, said means for entraining comprising a particle injection conduit intersecting the nozzle at a point adjacent the nozzle throat wherein said plasma stream is of relatively higher density, and means for feeding said particles through said conduit and through the boundary layer of said plasma stream toward the center thereof whereby both transferred kinetic energy and dwell time of the particles in the plasma stream are increased.

References Cited (Backward Citations)

US2982845A Cited
US3071678A Cited
US3183337A Cited
US3145287A Cited
US3179782A Cited
US3304402A Cited
US3313908A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-10-20 1979-04-21 1979-10-21 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-10-20 1983-04-21 1983-10-21 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-10-20 1987-04-21 1987-10-21 $7700.00 Window Closed / Lapsed

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