Flame spraying process and apparatus

• US 20070113781A1
• Filed: 11/04/2005
• Published: 05/24/2007
• Est. Priority Date: 11/04/2005
• Status: Abandoned Application

• Current Assignee: GJL Patents, LLC
• Original Assignee: GJL Patents, LLC
• Inventors: Lichtblau, George
• Application Number:
  US11/267,694
• Publication Number:
  US 20070113781A1
• Time in Patent Office: Days
• US Class Current: 118/620
• CPC Class Codes: C23C 4/129 Flame spraying
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A process, apparatus and material composition for forming a coherent refractory mass on a surface wherein one or more non-combustible materials are mixed with one or more metallic combustible powders and an oxidizer, igniting the mixture in a combustion chamber so that the combustible metallic particles react in an exothermic manner with the oxidizer and release sufficient heat to form a coherent mass of material under the action of the heat of combustion, and projecting this mass against the surface so that the mass adheres durably to the surface. The combustion chamber can be operative with a reverse vortex to cool the walls of the chamber.

Claims

1. Apparatus for forming a coherent refractory mass on a surface, the apparatus comprising:

a combustion chamber adapted to be disposed on a surface;

a container for holding metallic combustible powder(s) and non-combustible ceramic powder(s);

a first supply line for transporting one or more metallic combustible powders, one or more non-combustible powders and an oxidizer to the combustion chamber;

a second supply line for supplying air to the combustion chamber to supply additional oxygen, to assist in projecting the refractory mass from the combustion chamber and for cooling the inside of the combustion chamber; and

an igniter associated with the combustion chamber and operative to ignite the combustible powder, non-combustible material and oxidizer in the combustion chamber to cause the metallic combustible powder to react in an exothermic manner with the oxygen and release sufficient heat to form a refractory mass which is projected against the surface so that the mass adheres durable to the surface.

2. The apparatus of claim 1 wherein the first supply line includes a gas carrier for transporting the combustible and ceramic powder from the container to the combustion chamber.

3. The apparatus of claim 1 wherein the igniter is an electric arc.

4. The apparatus of claim 1 wherein the igniter is a gas pilot light.

5. The apparatus of claim 1 wherein the igniter is a plasma arc.

6. The apparatus of claim 2 wherein the gas carrier is air, oxygen or a combination of the two.

7. The apparatus of claim 1 wherein the rate of deposition of the coherent mass onto the surface is controlled by the rate of movement between the surface and the exit of the combustion chamber or vice-versa.

8. The apparatus of claim 1 wherein the combustion chamber is made of a ceramic material.

9. The apparatus of claim 1 wherein the combustion chamber contains openings into which a gas is injected to prevent the combustion products from contacting the inside surface of the combustion chamber and binding thereto.

10. The apparatus of claim 9 wherein the gas is air.

11. The apparatus of claim 1 wherein the combustion chamber is made of metal that is coated on the inside with a high temperature ceramic coating.

12. The apparatus of claim 1 wherein the second supply line causes a reverse vortex to form inside the combustion chamber in order to insulate the walls of the combustion chamber from the heat of combustion.

13. The apparatus of claim 12 wherein the chamber is substantially frustum-shaped.

14. The apparatus of claim 12 wherein the chamber is substantially a cylinder.

15. The apparatus of claim 13 wherein the combustion chamber has a closed end and an open end, and wherein the first supply line injects one or more metallic combustible powders, one or more non-combustible materials and an oxidizer into the closed end of the combustion chamber and substantially along the axis of the frustum.

16. The apparatus of claim 14 wherein the combustion chamber has a closed end and an open end, and wherein the first supply line injects one or more metallic combustible powders, one or more non-combustible materials and an oxidizer into the closed end of the cylinder and substantially along the axis of the cylinder.

17. The apparatus of claim 12 wherein the apparatus for creating a reverse vortex consists of a gas flow which flows circumferentially along the inside surface of the combustion chamber and travels from the open end to the closed end of the combustion chamber.

18. The apparatus of claim 12 wherein the apparatus for creating circumferential gas flow comprises a gas supply and one or more gas inlet nozzles oriented tangentially relative to the inside wall of the combustion chamber.

19. The apparatus of claim 18 wherein the gas inlet nozzles are located approximately at the open end of the combustion chamber.

20. The apparatus of claim 18 wherein the gas inlet nozzles are located approximately at the closed end of the combustion chamber.

21. The apparatus of claim 18 wherein the gas inlet nozzles are located at both the open and closed portions of the combustion chamber.

22. The apparatus of claim 1 wherein the igniter is located off of the center axis of the combustion chamber.

23. The apparatus of claim 1 wherein the igniter is located on the center axis of the combustion chamber.

24. The apparatus of claim 17 wherein said circumferential flow generates an axially-symmetric circumferential fluid flow.

25. The apparatus of claim 1 where the first supply line injects one or more metallic combustible powders, one or more non-combustible materials and an oxidizer into a reverse vortex port at the open end of the combustion chamber.

26. The apparatus of claim 1 where the second supply line injects one or more metallic combustible powders, one or more non-combustible materials and an oxidizer into a reverse vortex port at the open end of the combustion chamber.

27. The apparatus of claim 25 wherein the oxidizer is either air or oxygen.

28. The apparatus of claim 26 wherein the oxidizer is either air or oxygen.

29. The apparatus of claim 13 wherein the combustion chamber has a closed end which is shaped so as to increase the angular velocity of the air stream as it changes direction from a reverse vortex to a direct vortex from the closed end to an open end of the combustion chamber.

30. The apparatus of claim 14 wherein the combustion chamber has a closed end which is shaped so as to increase the angular velocity of the air stream as it changes direction from a reverse vortex to a direct vortex from the closed end to an open end of the combustion chamber.

31. The apparatus of claim 1 wherein the container is a volumetric screw feeder used for the metering of dry solids into a process.

32. The apparatus of claim 1 wherein the rate of delivery of the combustible and non-combustible powder is controlled by a screw conveyor driven by a variable speed motor.

33. The apparatus of claim 1 wherein the rate of delivery of the combustible and non-combustible powder is controlled by means of a variable valve which controls a gas carrier.

34. The apparatus of claim 33 wherein the gas carrier is air, oxygen or a combination of the two.

35. The apparatus of claim 31 wherein the output of the screw feeder is in fluid communication with the container holding the combustible and non-combustible powders.

36. The apparatus of claim 31 wherein the container holding the combustible and non-combustible powders is sealed from atmospheric pressure.

37. The apparatus of claim 1 wherein the combustion chamber is cylindrical in shape, is formed from two concentric shells with the space between the shells fully enclosed and in fluid communication with the interior portion of the combustion chamber.

38. The apparatus of claim 37 wherein one end of the combustion chamber is closed to prohibit the exhaust of the combustion products and one end is open to permit the exhaust of the combustion products.

39. The combustion chamber of claim 38 wherein the second supply line injects one or more metallic combustible powders, one or more non-combustible materials and an oxidizer into the space between the inner and outer shells of the combustion chamber to causes a forward vortex to form in the space between the inner and outer shells of the combustion chamber wherein the vortex travels in the direction from the closed end to the open end of the combustion chamber.

40. The apparatus of claim 39 wherein the forward vortex is in fluid communication with the central portion of the combustion chamber and causes a reverse vortex to flow circumferentially along the inside surface of the central portion of the combustion chamber and to travel in the direction from the open end to the closed end of the combustion chamber.

41. The apparatus of claim 38 wherein the second supply line injects air, oxygen or a combination of both into the space between the inner and outer shells of the combustion chamber to causes a forward vortex to form in the space between the inner and outer shells of the combustion chamber wherein the vortex travels in the direction from the closed end to the open end of the combustion chamber.

42. The apparatus of claim 41 wherein the forward vortex is in fluid communication with the central portion of the combustion chamber and causes a reverse vortex to flow circumferentially along the inside surface of the central portion of the combustion chamber and to travel in the direction from the open end to the closed end of the combustion chamber.

43. The apparatus of claim 38 wherein the first supply line injects one or more metallic combustible powders, one or more non-combustible materials and an oxidizer into the closed end of the combustion chamber.

44. The apparatus of claim 38 wherein the igniter is located on the central axis of the combustion chamber and at the closed end.

45. The apparatus of claim 38 wherein the flame from the igniter is directed tangential to the surface of the inner wall of the central portion of the combustion chamber and in proximity to the open end of the combustion chamber.

46. Apparatus for forming a coherent refractory mass on a surface, the apparatus comprising:

a combustion chamber adapted to be disposed on a surface;

a container for holding metallic combustible powder(s) and non-combustible ceramic powder(2);

a single supply line for transporting one or more metallic combustible powders, one or more non-combustible powders and an oxidizer to the combustion chamber; and

an igniter associated with the combustion chamber and operative to ignite the combustible powder, non-combustible powder and oxidizer in the combustion chamber to cause the metallic combustible powder to react in an exothermic manner with the oxidizer and release sufficient heat to form a refractory mass which is projected against the surface so that the mass adheres durable to the surface.

47. The apparatus of claim 46 wherein one end of the combustion chamber is closed to prohibit the exhaust of the combustion products and one end is open to enable the exhaust of the combustion products.

48. The apparatus of claim 46 wherein the igniter is an electric arc.

49. The apparatus of claim 46 wherein the igniter is a gas pilot light.

50. The apparatus of claim 46 wherein the igniter is a plasma arc.

51. The apparatus of claim 46 wherein the rate of delivery of the combustible and non-combustible powder(s) is controlled by a screw conveyor driven by a variable speed motor and a variable valve which controls the rate of delivery of air, oxygen or a combination of the two.

52. The apparatus of claim 46 wherein the rate of deposition of the coherent mass onto the surface is controlled by the rate of movement between the surface and the exit of the combustion chamber or vice-versa.

53. The apparatus of claim 46 wherein the combustion chamber is made of a ceramic material.

54. The apparatus of claim 46 wherein the combustion chamber is made of metal that is coated on the inside with a high temperature ceramic coating.

55. The apparatus of claim 46 wherein the supply line causes a reverse vortex to form inside the combustion chamber in order to insulate the walls of the combustion chamber from the heat of combustion.

56. The apparatus of claim 46 wherein the chamber is substantially a cylinder.

57. The apparatus of claim 47 wherein the supply line injects one or more metallic combustible powders, one or more non-combustible materials and an oxidizer into the closed end of the combustion chamber and substantially along the axis of the chamber.

58. The apparatus of claim 55 wherein the apparatus for creating a reverse vortex consists of a gas flow which flows circumferentially along the inside surface of the combustion chamber and travels from the open end to the closed end of the combustion chamber.

59. The apparatus of claim 55 wherein the apparatus for creating circumferential gas flow comprises a gas supply and one or more gas inlet nozzles oriented tangentially relative to the inside wall of the combustion chamber.

60. The apparatus of claim 59 wherein the gas inlet nozzles are located approximately at the open end of the combustion chamber.

61. The apparatus of claim 59 wherein the gas inlet nozzles are located approximately at the closed end of the combustion chamber.

62. The apparatus of claim 59 wherein the gas inlet nozzles are located at both the open and closed portions of the combustion chamber.

63. The apparatus of claim 46 wherein the igniter is located off of the center axis of the combustion chamber.

64. The apparatus of claim 46 wherein the igniter is located on the center axis of the combustion chamber.

65. The apparatus of claim 59 wherein said circumferential flow generates an axially-symmetric circumferential fluid flow.

66. The apparatus of claim 47 where the supply line injects one or more metallic combustible powders, one or more non-combustible materials and an oxidizer into a reverse vortex port at the open end of the combustion chamber and causes a reverse vortex to form inside the combustion chamber.

67. The apparatus of claim 47 wherein the closed end of the combustion chamber is shaped so as to increase the angular velocity of the air stream as it changes direction from a reverse vortex to a direct vortex from the closed end to the open end of the combustion chamber.

68. The apparatus of claim 46 wherein the container is a volumetric screw feeder used for the metering of dry solids into a process.

69. The apparatus of claim 68 wherein the rate of delivery of the combustible and non-combustible powder is controlled by a screw conveyor driven by a variable speed motor.

70. The apparatus of claim 46 wherein the rate of delivery of the combustible and non-combustible powder is controlled by means of a variable valve which controls a gas carrier.

71. The apparatus of claim 70 wherein the gas carrier is air, oxygen or a combination of the two.

72. The apparatus of claim 68 wherein the output of the screw feeder is in fluid communication with the container holding the combustible and non-combustible powders.

73. The container of claim 68 wherein the container holding the combustible and non-combustible powders is sealed from atmospheric pressure.

74. The combustion chamber of claim 46 wherein the combustion chamber is cylindrical in shape, is formed from two concentric shells with the space between the shells fully enclosed and in fluid communication with the central portion of the combustion chamber.

75. The apparatus of claim 74 wherein one end of the combustion chamber is closed to prohibit the exhaust of the combustion products and one end is open to permit the exhaust of the combustion products.

76. The apparatus of claim 75 wherein the supply line injects one or more metallic combustible powders, one or more non-combustible materials and an oxidizer into the space between the inner and outer shells of the combustion chamber to causes a forward vortex to form in the space between the inner and outer shells of the combustion chamber wherein the vortex travels in the direction from the closed end to the open end of the combustion chamber.

77. The combustion chamber of claim 76 wherein the forward vortex is in fluid communication with the central portion of the combustion chamber and causes a reverse vortex to flow circumferentially along the inside surface of the central portion of the combustion chamber and to travel in the direction from the open end to the closed end of the combustion chamber.

78. The apparatus of claim 75 wherein the supply line injects one or more metallic combustible powders, one or more non-combustible materials and an oxidizer into the closed end of the combustion chamber.

79. The apparatus of claim 75 wherein the supply line injects a portion of the metallic combustible powders and non-combustible materials and the oxidizer into the closed end of the combustion chamber and the remainder of the metallic combustible powders and non-combustible materials and oxidizer into the space between the inner and outer walls of the combustion chamber.

80. The apparatus of claim 79 wherein that portion of the combustible powder and non-combustible materials and oxidizer that is injected into the space between the inner and outer walls of the combustion chamber causes a forward vortex of gas and materials which flows circumferentially from the closed end towards the open end of the combustion chamber.

81. The combustion chamber of claim 75 wherein the igniter is located on the central axis of the combustion chamber and at the closed end.

82. The combustion chamber of claim 75 wherein the flame from the igniter is directed tangential to the surface of the inner wall of the central portion of the combustion chamber and in proximity to the open end of the combustion chamber.