Process of removing a ceramic coating deposit in a surface hole of a component
A process of removing ceramic deposits from a surface hole in a component, a particular example being portions of a ceramic coating deposited on a surface of a component equipped with cooling holes. The process makes use of a pulsed Nd:YAG laser operated with parameters that avoid delamination, cracking or otherwise damaging a ceramic coating surrounding a cooling hole. The laser is operated to generate a laser beam that removes some of the ceramic deposit from the hole while a residual portion of the ceramic deposit remains surrounding the hole to define a surface opening.
1. A process of removing a ceramic deposit from a surface hole of a component having a ceramic coating on a surface thereof, the process comprising the steps of:
positioning an Nd:YAG laser generator so that a laser beam generated by the generator is directed at the programmed location of the hole used during installation of the hole; and then
directing a pulsed laser beam at the programmed location of the hole to remove the ceramic deposit from the hole, the pulsed laser beam having a diameter less than the hole at the surface of the component, a pulse width of about 0.25 to about 6.0 milliseconds, and a pulse frequency of about 2 to about 20 Hz,
wherein some of the ceramic deposit is removed from the hole and a residual portion of the ceramic deposit remains surrounding the hole to define a surface opening without substantial delamination or cracking of the ceramic coating surrounding the hole.
2. A process according to claim 1 , wherein the ceramic coating has a thickness of greater than 0.5 mm.
3. A process according to claim 1 , wherein the ceramic coating has a thickness of greater than 0.75 mm.
4. A process according to claim 1 , wherein the hole has a diameter of greater than 0.25 mm and the pulsed laser beam has a pulse width of about 0.4 to about 1.0 milliseconds and a pulse frequency of about 6 to about 16 Hz.
5. A process according to claim 1 , wherein the hole has a diameter of less than 0.25 mm.
6. A process according to claim 1 , further comprising the steps of:
prior to the positioning step, installing the hole in the component at the programmed location of the hole; and then
depositing the ceramic coating on the surface and the deposit in the surface hole.
7. A process according to claim 1 , wherein removal of the deposit is by thermal evaporation.
8. A process according to claim 1 , wherein the ceramic coating is deposited by plasma spraying.
9. A process according to claim 1 , wherein the component is a gas turbine engine component.
10. A process of forming cooling holes that intersect a surface of an air-cooled gas turbine engine component, the process comprising the steps of:
installing the holes in the component at programmed locations for the holes;
depositing a ceramic coating on the surface of the component so as to also deposit a ceramic deposit in the hole;
heat treating the component in a vacuum to reduce residual stresses in the ceramic coating;
positioning an Nd:YAG laser generator so that a laser beam generated by the generator is directed at one of the programmed locations of one of the holes; and then
directing a pulsed laser beam at the programmed location of the hole to evaporate the ceramic deposit from the hole, the pulsed laser beam being focused to have a diameter less than the diameter of the hole at the surface of the component, the pulsed laser beam having a pulse width of about 0.25 to about 6.0 milliseconds and a pulse frequency of about 2 to about 20 Hz,
wherein some of the ceramic deposit is removed from the hole and a residual portion of the ceramic deposit remains surrounding the hole to define a surface opening without substantial delamination or cracking of the ceramic coating surrounding the hole.
11. A process according to claim 10 , further comprising the step of, prior to the depositing step, depositing a metallic bond coat on the surface of the component, wherein the ceramic coating is deposited on the bond coat.
12. A process according to claim 11 , wherein the bond coat is a diffusion aluminide.
13. A process according to claim 10 , wherein the ceramic coating is deposited by plasma spraying.
14. A process according to claim 10 , wherein the heat treating step is performed at a temperature of about 1025° C. to about 1125° C. for about two to about eight hours.
15. A process according to claim 10 , wherein the ceramic coating has a thickness of greater than 0.5 mm.
16. A process according to claim 10 , wherein the ceramic coating has a thickness of greater than 0.75 mm.
17. A process according to claim 10 , wherein the holes have diameters of greater than 0.25 mm and the pulsed laser beam has a pulse width of about 0.55 to about 0.75 milliseconds and a pulse frequency of about 13 to about 17 Hz.
18. A process according to claim 17 , wherein the pulsed laser beam has a pulse width of about 0.65 milliseconds and a pulse frequency of about 15 Hz.
19. A process according to claim 10 , wherein the holes have diameters of less than 0.25 mm and the pulsed laser beam has a pulse width of about 0.55 to about 0.75 milliseconds and a pulse frequency of about 13 to about 17 Hz.
20. A process according to claim 19 , wherein the pulsed laser beam has a pulse width of about 0.65 milliseconds and a pulse frequency of about 15 Hz.