Oxidation resistant thermal barrier coating system for combustor panels
An oxidation resistant coating system for a turbine engine component includes a cathodic arc coating applied to a surface of the engine component, a thin APS metallic coating applied to a surface of the cathodic arc coating, and a ceramic top coating applied to a surface of the thin APS metallic coating to improve lifetime of the engine components.
1. A coating system for an article, comprising:
a first oxidation resistant metallic coating applied to a surface of the article, wherein the first metallic coating is in continuous contact with the contiguous surface of the article, is formed by cathodic arc deposition in a vacuum, and the first metallic coating has a surface;
a second metallic coating applied to the whole surface of the first metallic coating, wherein the second metallic coating is applied by air plasma spray (APS) and the second metallic coating has a surface; and
a ceramic top coating applied to the surface of the second metallic coating.
2. The coating system of claim 1 , wherein said article includes a combustor panel of a gas turbine engine.
3. The coating system of claim 1 , wherein the composition of the first metallic coating includes nickel, chromium, or an alloy of nickel and chromium.
4. The coating system of claim 1 , wherein the composition of the second metallic coating includes nickel, chromium, or an alloy of nickel and chromium.
5. The coating system of claim 1 , wherein the first metallic coating has the same composition as that of the second metallic coating.
6. The coating system of claim 1 , wherein the surface of the second metallic coating has a higher surface roughness than the surface of the first metallic coating and provides a mechanical interlocking between the second metallic coating and the ceramic top coating.
7. The coating system of claim 1 , wherein the ceramic top coating is formed by an air plasma spray (APS).
8. A coated article, comprising:
an article having at least one surface;
a first metallic coating in continuous contact with the contiguous surface of the article and applied to the surface of the article by cathodic arc deposition in a vacuum;
a second metallic coating applied to the whole surface of the first metallic coating, and formed by an air plasma spray (APS); and
a ceramic top coating applied to the whole surface of the second metallic coating, wherein the second metallic coating is of a similar metallic composition to the first metallic coating.
9. The coated article of claim 8 , wherein said article includes combustor panels of a gas turbine engine.
10. The coated article of claim 8 , wherein a composition of the first metallic coating includes nickel, chromium, or an alloy of nickel and chromium.
11. The coated article of claim 8 , wherein a composition of the second metallic coating includes nickel, chromium, or an alloy of nickel and chromium.
12. The coated article of claim 8 , wherein the second metallic coating has the same composition as that of the first metallic coating.
13. The coated article of claim 8 , wherein the second metallic coating surface has a higher surface roughness than the first metallic coating surface and the second metallic coating surface provides a mechanical interlocking between the APS metallic coating and the ceramic top coating.
14. The coated article of claim 8 , wherein the ceramic top coating is formed by an air plasma spray (APS) in an atmospheric pressure.
15. A process for forming an oxidation resistant coating on an article, comprising:
providing a metal substrate;
forming an oxidation resistant coating on a surface of the metal substrate by cathodic arc deposition in a vacuum wherein the oxidation resistant coating is in continuous contact with the contiguous surface of the metal substrate;
forming a metallic coating on the whole surface of the cathodic arc deposited coating by an air plasma spray (APS); and
forming a ceramic top coating on the whole surface of the metallic coating, wherein the metallic coating is of a similar metallic composition to the oxidation resistant coating.
16. The process of claim 15 , wherein a composition of the oxidation resistant coating includes nickel, chromium, or an alloy of nickel and chromium.
17. The process of claim 15 , wherein a composition of the metallic coating includes nickel, chromium, or an alloy of nickel and chromium.
18. The process of claim 15 , wherein said article includes combustor panels of a gas turbine engine.
19. The processes of claim 15 , wherein the oxidation resistant coating has the same composition as that of the metallic coating.
20. The process of claim 15 , wherein the ceramic top coating is formed by an air plasma spray (APS) in an atmospheric pressure.