Maskant for use in aluminizing a turbine component
View Patent ↗A mask is used in aluminizing of superalloy turbine component, such as a turbine blade, where a region exposed to relatively high operating temperature is aluminized to form a diffusion aluminide coating and another region exposed to relatively lower operating temperatures is masked to prevent aluminizing of the masked region while concurrently being enriched in Cr and/or retaining a pre-existing Cr-content from the superalloy chemistry itself or from a previous chromizing operation.
1. A mask for preventing aluminizing of a region of a component made of a superalloy, comprising a mixture of chromium-containing powder, nickel-containing powder and refractory powder wherein the chromium-containing powder comprises metallic chromium powder or chromium-containing metal alloy powder, the chromium-containing powder being present in the mixture in an amount greater than about 10 weight % effective (a) to supply chromium to form a chromium-enriched surface on the superalloy component beneath the mask during aluminizing of an unmasked region or (b) to supply chromium to a pre-existing chromium-enriched chromized surface on the superalloy component beneath the mask to retain the chromium-enriched chromized surface during aluminizing of an unmasked region.
2. The mask of claim 1 wherein the chromium-containing metal alloy powder comprises an alloy of Cr and a transition metal.
3. The mask of claim 1 wherein the chromium-containing powder is present in the mask in an amount to provide a Cr chemical activity in the mask that is greater than the Cr activity of the superalloy or of the pre-existing Cr-enriched chromized surface.
4. The mask of claim 1 wherein the Cr content is less than about 25 weight % of the weight of the mixture.
5. A method of aluminizing a nickel base superalloy component, comprising masking a region of the component with the mask of claim 1 and exposing an unmasked region to a gaseous aluminizing atmosphere to form a diffusion aluminide coating thereon while (a) forming the chromium-enriched surface beneath the mask during aluminizing of the unmasked region or (b) retaining the chromium-enriched chromized surface beneath the mask during aluminizing of the unmasked region.
6. The method of claim 5 wherein the mask forms the chromium-enriched surface that comprises alpha chromium phase.
7. The method of claim 6 wherein the chromium-enriched surface comprises a layer of the alpha chromium phase and an underlying zone enriched in solid solution chromium beneath the layer.
8. The method of claim 5 wherein the mask forms the chromium-enriched surface that comprises a solid solution chromium-enriched zone on the superalloy component.
9. A mask for preventing aluminizing of a region of a component made of a superalloy, comprising an inner mask comprising metallic chromium powder or chromium-containing metal alloy powder and an outer mask on the inner mask wherein the outer mask comprises a mixture of chromium-containing powder, nickel-containing powder, and refractory powder and wherein the chromium-containing powder of the outer mask comprises metallic chromium powder or chromium-containing metal alloy powder and wherein the collective amount of chromium in the inner mask and the outer mask is effective (a) to supply chromium to form a chromium-enriched surface on the superalloy component beneath the mask during aluminizing of an unmasked region or (b) to supply chromium to a pre-existing chromium-enriched chromized surface on the superalloy component beneath the mask to retain the chromium-enriched chromized surface during aluminizing of an unmasked region.
10. The mask of claim 9 wherein the Cr-containing metal alloy powder comprises an alloy of Cr and a transition metal.
11. The mask of claim 9 wherein the Cr content of the mixture of the outer mask is greater than 10 weight % of the weight of the mask.
12. The mask of claim 11 wherein the Cr content of the mixture of the outer mask is less than about 25 weight % of the weight of the mask.
13. The mask of claim 9 wherein the inner mask is free of activator and refractory powder.
14. A method of aluminizing a nickel base superalloy component, comprising masking a region of the component with the mask of claim 9 and exposing an unmasked region to a gaseous aluminizing atmosphere to form a diffusion aluminide coating thereon while (a) forming the chromium-enriched surface beneath the mask during aluminizing of the unmasked region or (b) retaining the chromium-enriched chromized surface beneath the mask during aluminizing of the unmasked region.
15. The method of claim 14 wherein the mask forms the chromium-enriched surface that comprises alpha chromium phase.
16. The method of claim 15 wherein the chromium-enriched surface comprises a layer of the alpha chromium phase and an underlying zone enriched in solid solution chromium beneath the layer.
17. The method of claim 14 wherein the mask forms the chromium-enriched surface that comprises a solid solution chromium-enriched zone on the superalloy component.