IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0976969
(2004-10-29)
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등록번호 |
US-8367967
(2013-02-05)
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발명자
/ 주소 |
- Zajchowski, Paul H.
- Blankenship, Donn
- Shubert, Gary C.
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출원인 / 주소 |
- United Technologies Corporation
|
인용정보 |
피인용 횟수 :
0 인용 특허 :
21 |
초록
▼
A method and apparatus for repairing a thermal barrier coating on components in gas turbine engines and the like. The apparatus includes a microplasma spray gun having an anode, cathode, and an arc generator for generating an electric arc between the anode and cathode. The apparatus includes a nozzl
A method and apparatus for repairing a thermal barrier coating on components in gas turbine engines and the like. The apparatus includes a microplasma spray gun having an anode, cathode, and an arc generator for generating an electric arc between the anode and cathode. The apparatus includes a nozzle for emitting arc gas into the electric arc. The electric arc is operable for ionizing the gas to create a plasma gas stream. A powder injector injects powdered thermal barrier coating material into the plasma gas stream. Defective areas of the thermal barrier coating can be patched on the component without masking the component.
대표청구항
▼
1. A microplasma spray apparatus for repairing a thermal barrier coating on components in a gas turbine engine, comprising: a microplasma gun including an anode, a cathode, and an arc generator for generating an electric arc between the anode and cathode;a nozzle for emitting arc gas into the electr
1. A microplasma spray apparatus for repairing a thermal barrier coating on components in a gas turbine engine, comprising: a microplasma gun including an anode, a cathode, and an arc generator for generating an electric arc between the anode and cathode;a nozzle for emitting arc gas into the electric arc, the electric arc operable for ionizing the gas to create a plasma gas stream; anda powder injector for injecting powdered thermal barrier coating material into the plasma gas stream and patching a defective area of the thermal barrier coating, the thermal barrier coating being applied without masking any portion of the component or stripping a remaining non-defective thermal barrier coating on the component,wherein said cathode includes an electrode extending therefrom and disposed through an aperture of said nozzle, and said anode is disposed opposite said cathode within an anode holder mounted to an exterior surface of said microplasma gun. 2. The microplasma spray apparatus of claim 1, wherein the microplasma gun operates at a relatively low power range between approximately 0.5 Kilowatts and 2.5 Kilowatts. 3. The microplasma spray apparatus of claim 1, wherein the microplasma gun is operable for applying the thermal barrier coating to thin walled portions of the component without distorting the component. 4. The microplasma spray apparatus of claim 1, wherein a maximum surface temperature of the component caused by the coating process is approximately 200 degrees F. 5. The microplasma spray apparatus of claim 1, wherein the microplasma gun applies the thermal barrier coating material in narrow widths of approximately 2 mm to the component. 6. The microplasma spray apparatus of claim 1, wherein the arc gas flow rate is between approximately 1.5 and 3 liters per minute. 7. The microplasma spray apparatus of claim 1, wherein the arc gas is inert. 8. The microplasma spray apparatus of claim 1, wherein the arc gas is argon. 9. The microplasma spray apparatus of claim 1, further including a shield gas cap having shielding gas injected therethrough. 10. The microplasma spray apparatus of claim 9, wherein the shielding gas flow rate is between approximately 2 and 4 liters per minute. 11. The microplasma spray apparatus of claim 9, wherein the shielding gas is inert. 12. The microplasma spray apparatus of claim 9, wherein the shielding gas is argon. 13. The microplasma spray apparatus of claim 1, wherein the thermal barrier coating includes at least one layer of metal and ceramic based materials. 14. The microplasma spray apparatus of claim 13, wherein the thermal barrier coating material includes a “M”CrA1Y bond layer and a stabilized zirconia based ceramic top layer. 15. The microplasma spray apparatus of claim 1, further including a powder hopper for holding the powdered thermal barrier coating material prior to the powdered thermal barrier coating material being injected into the plasma gas stream. 16. The microplasma spray apparatus of claim 1, wherein the powder feed rate is approximately between 1 and 30 grams per minute. 17. The microplasma spray apparatus of claim 1, further including a cooling system for cooling hot portions of the of the microplasma gun. 18. The microplasma spray apparatus of claim 1, wherein the microplasma gun applies the coating from a distance to the component of between approximately 1.5 inches to 6.5 inches. 19. The microplasma spray apparatus of claim 1, wherein the microplasma spray angle relative to a normal axis of the component is approximately between a positive 45 degree angle and a negative 45 degree angle. 20. The microplasma spray apparatus of claim 1, wherein the microplasma gun generates a noise level of between approximately 40 and 70 decibels. 21. The microplasma spray apparatus of claim 1, further including a cathode shroud surrounding a portion of the cathode. 22. The microplasma spray apparatus of claim 21, further including a shield gas cap substantially encompassing the cathode shroud, the shield gas cap operable for providing shielding gas as a barrier between the arc gas and an ambient atmosphere. 23. The microplasma spray apparatus of claim 22, further including a shield cap insulator positioned between the shield gas cap and the cathode shroud. 24. The microplasma spray apparatus of claim 1, wherein the microplasma gun is hand held. 25. The microplasma spray apparatus of claim 1, wherein the component is a turbine blade. 26. The microplasma spray apparatus of claim 1, wherein the component is a turbine vane. 27. The microplasma spray apparatus of claim 1, wherein the component is a combustor liner. 28. The microplasma spray apparatus of claim 1, wherein the component is an exhaust nozzle. 29. The microplasma spray apparatus of claim 1, wherein the component is exposed to high operating temperatures caused by combustion exhaust gas. 30. A method for repairing a thermal barrier coating on a workpiece with a microplasma spray apparatus, comprising: providing a microplasma gun including an anode and a cathode, said anode disposed opposite said cathode with an anode holder mounted to an exterior surface of said microplasma gun;injecting inert arc gas from a nozzle;generating an electric arc between the anode and the cathode through the arc gas;ionizing the arc gas with the electric arc to form a plasma gas stream;injecting powdered thermal barrier coating material into the plasma gas stream;coating a localized area of the workpiece with thermal barrier coating material without masking the workpiece; andpatching a defective area of the thermal barrier coating without stripping the remaining non-defective thermal barrier coating on the workpiece. 31. The method of claim 30, further including operating the microplasma gun at a relatively low power range between approximately 0.5 Kilowatts and 2.5 Kilowatts. 32. The method of claim 30, further including applying the coating material to the workpiece without causing distortion of the workpiece. 33. The method of claim 30, further including applying the coating material to the workpiece in narrow widths of approximately 2 mm. 34. The method of claim 30, further including flowing the arc gas at a rate between approximately 1.5 and 3 liters per minute. 35. The method of claim 30, further including flowing the shielding gas at a rate between approximately 2 and 4 liters per minute. 36. The method of claim 30, further including feeding the powder material at a rate between approximately 1 and 30 grams per minute. 37. The method of claim 30, further including cooling the microplasma gun with a fluid cooling system. 38. The method of claim 37, wherein the cooling fluid is at least partially water based. 39. The method of claim 30, further including applying the coating to the workpiece from a distance of between approximately 1.5 to 6.5 inches. 40. The method of claim 30, further including generating a noise level of between approximately 40 and 70 decibels during operation. 41. The method of claim 30, further including patching the thermal barrier coating with a hand held microplasma spray gun. 42. A method for repairing the thermal barrier coating of a gas turbine components with a microplasma spray coating apparatus, comprising: using a hand controlled and operated microplasma spray gun including an anode and a cathode, said anode disposed opposite said cathode with an anode holder mounted to an exterior surface of said microplasma gun;injecting inert arc gas through an electric arc generated by the spray gun;ionizing the arc gas with the electric arc to form a plasma gas stream;injecting powdered thermal barrier coating material into the plasma gas stream;spray coating a localized area of a component with the powdered thermal barrier coating material without masking the component and without utilizing a dedicated spray coating facility; andpatching a defective area of the thermal barrier coating without stripping the remaining non-defective thermal barrier coating on the component. 43. The method of claim 42, further including patching a defective area of the thermal barrier coating without stripping the remaining non-defective thermal barrier coating on the component and while the component remains installed on a gas turbine engine. 44. The method of claim 42, further including operating the microplasma gun at a relatively low power range between approximately 0.5 Kilowatts and 2.5 Kilowatts. 45. The method of claim 42, further including applying the coating material to the component without causing distortion of the component. 46. The method of claim 42, further including applying the coating material to the component in narrow widths of approximately 2 mm. 47. The method of claim 42, further including flowing the arc gas at a rate between approximately 1.5 and 3 liters per minute. 48. The method of claim 42, further including flowing the shielding gas at a rate between approximately 2 and 4 liters per minute. 49. The method of claim 42, further including feeding the powder material at a rate between approximately 1 and 30 grams per minute. 50. The method of claim 42, further including cooling the microplasma gun with a water cooling system. 51. The method of claim 42, further including applying the coating to the component from a distance of between approximately 1.5 to 6.5 inches. 52. The method of claim 42, further including generating a noise level of between approximately 40 and 70 decibels during operation.
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