Method and apparatus for ultra high velocity dual stream metal flame spraying

Claim 2

A flame spraying method comprising the steps of: forming a primary jet stream of melted material particles suspended in a very hot carrier gas, igniting a fuel/air mixture in an internal burner combustion chamber to create high pressure, high temperature products of combustion within the confined volume of the combustion chamber, discharging the hot products of combustion from said internal burner through a manifold nozzle closing off said combustion chamber as a converging annular flow from a circular series of closely spaced nozzle orifices or a narrow continuous slot of circumferential ring geometry including a diminished core section defining the inner envelope of said converging annular secondary jet stream, introducing said primary jet stream molten particles within said carrier gas upstream of and axially into the secondary jet stream in the direction of flow of said secondary jet stream, and controlling combustion within said internal burner to accelerate said molten particles to supersonic velocity and to thereby create an extended length small diameter stream of molten particles downstream of said manifold nozzle of extremely high particle density for rapid, high bonding strength molten particle deposition on a surface to be coated, while maintaining the temperature of the secondary jet stream at a sufficiently high value to prevent solidification of the molten particles prior to impact on said surface.

Claim 3

The flame spraying method as claimed in claim 1, wherein said step of forming a primary jet stream of melted material particles suspended in a carrier gas comprises suspending powdered material in said primary jet stream carrier gas and melting said powder to form said melted material particles.

Claim 4

The flame spraying method as claimed in claim 1, wherein said step of forming a primary jet stream of melted material particles suspended in a carrier gas comprises feeding of material in wire or rod form into the primary jet stream carrier gas, whose temperature is sufficient to melt said particles.

Claim 5

The flame spraying method as claimed in claim 1, wherein said step of forming a primary jet stream of melted material particles suspended in a carrier gas comprises the forming of an oxide-fuel or plasma flame jet of higher temperature than the secondary accelerating jet stream, and wherein said primary jet stream material particles are completely melted prior to introduction of said melted particles into said accelerating secondary jet stream.

Claim 6

The flame spraying method as claimed in claim 3, wherein said step of forming a primary jet stream of melted material particles suspended in a carrier gas comprises feeding two continuously moving wires or rods of electrically conductive metal into said stream of carrier gas along intersecting paths and striking an arc between the ends of said wires or rods to produce said molten particles within said primary jet stream for flow into said accelerating gas and secondary accelerating jet stream.

Claim 7

The flame spraying method as claimed in claim 1, wherein said step of forming a primary jet stream of melted material particles suspended in a carried gas comprises feeding of a single conductive wire or rod into a plasma arc for melting of said wire or rod material by the entrained gaseous flow prior to the primary jet stream gaseous flow carrying said molten particles to said converging annular secondary jet stream.

Claim 8

The flame spraying method as claimed in claim 1 or claim 6, wherein said step of forming a high velocity accelerating secondary jet stream comprises feeding of the products of combustion from a internal burner through a circular series of closely spaced or a continuous slot of circumferential ring geometry from reactants containing a greater percentage of oxygen than that contained in atmospheric air.

Claim 9

The flame spraying method as claimed in claim 7, further comprising the step of constraining the outer boundary of the converging annular secondary jet gaseous to cylindrical form having an elongated central core of relatively low velocity, and focussing the melted material particles into a small diameter cylindrical stream at the point of introduction of the melted material particles to the core region of said secondary accelerating jet stream.

Claim 10

The flame spraying method as claimed in claim 1, wherein the internal burner is operated at a pressure on the order of 100 psig to 600 psig, and the secondary jet stream is at a velocity of about 1000 to 4000 feet per second.

Claim 11

A flame spraying method comprising the steps of: establishing an arc column between an internal first electrode within a cylindrical plasma torch body and a constricting bore nozzle of said torch body, creating a plasma column annularly separated from the entry bore of an anode element downstream of the exit end of said constricting bore nozzle of said plasma torch body with said arc column passing at least axially part way through the exit bore of the anode element, passing a flow of powder or material to be melted into or near the exit of the plasma torch body nozzle bore and along said axial arc column in said primary jet stream, igniting a fuel/air mixture in an internal burner combustion chamber to create high pressure, high temperature products of combustion within the confined volume of the combustion chamber, causing the products of combustion of said internal burner to exit from said burner through a manifold nozzle closing off one end of the combustion chamber as a converging annular flow of gas from a circular series of closely spaced nozzle orifices or a continuous slot of circumferential ring geometry to form a gaseous accelerating secondary jet stream including a diminished core section defining the inner envlope of said converging annular secondary jet stream into said primary jet stream bearing said melted particles in the same direction of flow as said primary jet stream, and controlling combustion within said internal burner to accelerate said molten particles to supersonic velocity and to thereby create an extended length small diameter stream of molten particles downstream of said manifold nozzle of extreme high practice density for rapid, high bonding strength molten particle deposition on a surface to be coated, while maintaining the temperature of said secondary jet stream at a sufficiently high value to prevent solidification of the molten particles over said extended length necessary to reach supersonic velocity prior to impact on said surface.

Claim 12

A flame spraying method comprising the steps of: establishing an arc column between an internal first electrode within a cylindrical plasma torch body and a constricting bore nozzle of said torch body, creating a plasma column annularly separated from the entry bore of an anode element downstream of the exit end of said constricting bore nozzle of said plasma torch body with said arc column passing at least axially part way through the exit bore of the anode element, passing a flow of powder or material to be melted into or near the exit of the plasma torch body nozzle bore and along said axial arc column in said primary jet stream, igniting a fuel/air mixture in an internal burner combustion chamber to create high pressure, high temperature products of combustion within the confined volume of the combustion chamber, causing the products of combustion of said internal burner to exit from said burner through a manifold nozzle closing off one end of the combustion chamber as a converging annular flow of gas from a circular series of closely spaced nozzle orifices or a continuous slot of circumferential ring geometry to form a gaseous accelerating secondary jet stream including a diminished core section defining the inner envlope of said converging annular secondary jet stream into said primary jet stream bearing said melted particles in the same direction of flow as said primary jet stream, and controlling combustion within said internal burner to accelerate said molten particles to supersonic velocity and to thereby create an extended length small diameter stream of molten particles downstream of said manifold nozzle of extreme high practice density for rapid, high bonding strength molten particle deposition on a surface to be coated, while maintaining the temperature of said secondary jet stream at a sufficiently high value to prevent solidification of the molten particles over said extended length necessary to reach supersonic velocity prior to impact on said surface.

Claim 13

The flame spraying method as claimed in claim 10, wherein the internal burner is operated at a pressure on the order of 100 psig to 600 psig, and the secondary jet stream is at, a velocity of about 1000 to 4000 feet per second.

Claim 14

A supersonic velocity dual stream flame spraying apparatus, said apparatus comprising: a cylindrical plasma torch body including a constricting bore nozzle, means including said plasma torch body for forming a primary jet stream of melted material particles suspended in a very hot carrier gas and exiting from said constricting bore nozzle of said torch body, an internal burner having a combustion chamber, means for igniting a fuel/air mixture in said internal burner combustion chamber to create high pressure, high temperature products of combustion within the confined volume of said combustion chamber, said internal burner including a manifold nozzle closing off one end of said combustion chamber and having a circular series of closely spaced nozzle orifices or a continuous slot of circumferential ring geometry, said manifold nozzle being positioned downstream and spaced from said constricting bore nozzle of said torch bore body to create an annular gas aspirating passage intermediate of said constricting bore nozzle and said circular series of closely spaced nozzle orifices or said continuous slot of circumferential ring geometry concentrically surrounding the primary jet stream of the melted material particles suspended in the very hot carrier gas exiting from said torch body constricting bore nozzle for creating an accelerating secondary jet stream about said primary jet stream, said said secondary jet stream including a diminished core section defining the inner envelope of said converging annular secondary jet stream with said streams flowing in the same direction, and means for controlling combustion within said internal burner to accelerate said molten particles to supersonic velocity and to thereby create an extended length small diameter stream of molten particles downstreams of said manifold nozzle of extremely high density for rapid, high bonding strength molten particle deposition on a surface to be coated, while maintaining the temperature of said secondary jet stream at a sufficiently high value to prevent solidification of said molten particles prior to impact on said surface with said secondary accelerating jet stream aspirating gas flow through said annular passage preventing normal radial expansion of the plasma gas exiting from said plasma torch constricting bore nozzle by causing aspirated gases to converge in the direction of primary and secondary jet streams to squeeze both hot gas streams and the particles entrained therein to focus the stream of molten particles to a constant small diameter over said extended length.

Claim 15

A supersonic velocity dual stream flame spraying apparatus, said apparatus comprising: a cylindrical plasma torch body including a constricting bore nozzle, means including said plasma torch body for forming a primary jet stream of melted material particles suspended in a very hot carrier gas and exiting from said constricting bore nozzle of said torch body, an internal burner having a combustion chamber, means for igniting a fuel/air mixture in said internal burner combustion chamber to create high pressure, high temperature products of combustion within the confined volume of said combustion chamber, said internal burner including a manifold nozzle closing off one end of said combustion chamber and having a circular series of closely spaced nozzle orifices or a continuous slot of circumferential ring geometry, said manifold nozzle being positioned downstream and spaced from said constricting bore nozzle of said torch bore body to create an annular gas aspirating passage intermediate of said constricting bore nozzle and said circular series of closely spaced nozzle orifices or said continuous slot of circumferential ring geometry concentrically surrounding the primary jet stream of the melted material particles suspended in the very hot carrier gas exiting from said torch body constricting bore nozzle for creating an accelerating secondary jet stream about said primary jet stream, said said secondary jet stream including a diminished core section defining the inner envelope of said converging annular secondary jet stream with said streams flowing in the same direction, and means for controlling combustion within said internal burner to accelerate said molten particles to supersonic velocity and to thereby create an extended length small diameter stream of molten particles downstreams of said manifold nozzle of extremely high density for rapid, high bonding strength molten particle deposition on a surface to be coated, while maintaining the temperature of said secondary jet stream at a sufficiently high value to prevent solidification of said molten particles prior to impact on said surface with said secondary accelerating jet stream aspirating gas flow through said annular passage preventing normal radial expansion of the plasma gas exiting from said plasma torch constricting bore nozzle by causing aspirated gases to converge in the direction of primary and secondary jet streams to squeeze both hot gas streams and the particles entrained therein to focus the stream of molten particles to a constant small diameter over said extended length.

Claim 17

The ultra high velocity dual stream flame spraying apparatus as claimed in claim 12, further comprising means for operating the internal burner at a pressure on the order of 100 psig to 600 psig to provide a secondary jet stream velocity of about 1000 to 4000 feet per second.