Calcium-magnesium-alumino-silicate resistant thermal barrier coatings
A method for forming a coating system on a component includes depositing a reactive layer with predetermined CMAS reaction kinetics on at least a portion of a thermal barrier coating. The method also includes activating the reactive layer with a scanning laser. A component, such as a gas turbine engine component, includes a substrate, a thermal barrier coating and a reactive layer. The thermal barrier coating is deposited on at least a portion of the substrate. The reactive layer is deposited on at least a portion of the thermal barrier coating. The reactive layer has predetermined CMAS reaction kinetics activated by laser scanning.
1. A method for forming a coating system on a metallic component comprising:
depositing a reactive layer comprising a CMAS powder mixture with predetermined calcium-magnesium-alumino-silicate (CMAS) reaction kinetics on at least a portion of a thermal barrier coating; and
activating the reactive layer with a laser, wherein activating the reactive layer comprises chemically reacting the CMAS powder mixture and a portion of the thermal barrier coating and fusing the reactive layer and at least a portion of the thermal barrier coating.
2. The method as recited in claim 1 , further comprising forming the thermal barrier coating from a stabilized zirconia.
3. The method as recited in claim 1 , further comprising forming the thermal barrier coating from a stabilized zirconia having at least one crystallization promoting material selected from the group consisting of La 2 Zr 2 O 7 , GD 2 Zr 2 O 7 , Al 2 O 3 , TiO 2 , Y 2 Zr 2 O 7 , and mixtures thereof.
4. The method as recited in claim 1 , further comprising depositing a bond coat on a surface of a substrate followed by depositing the thermal barrier coating onto the bond coat.
5. The method as recited in claim 1 , wherein depositing the reactive layer includes depositing chemically conditioned CMAS and at least one reactive material selected from the group consisting of Y 2 Zr 2 O 7 and TiO 2 .
6. The method as recited in claim 1 , wherein the activated reactive layer has a melting temperature higher than the melting temperature of environmental CMAS.
7. The method as recited in claim 6 , wherein the CMAS powder mixture comprises chemically conditioned CMAS and Y 2 Zr 2 O 7 .
8. The method as recited in claim 6 , wherein the activated reactive layer melting temperature is at least 50 degrees Fahrenheit (10 degrees Celsius) higher than the melting temperature of environmental CMAS.