Low cost chrome and chrome/aluminide process for moderate temperature applications
A low cost chromide and chromide/aluminide process for moderate temperature applications. A gas turbine engine component is cleaned and coated with a layer of metal, generally chromium or chromium and aluminum, containing paint. The metal containing paint layer is heated to a first temperature for a first period of time in an air environment to volatilize the solvents in the paint. The metal containing paint layer is heated to a second temperature for a second period of time in an oxygen-free atmosphere to volatilize the solvents in the paint. The now metal layer and component are heated to a third temperature for a third period of time to interdiffuse the metal and the metal of the component. The component and diffusion layer are then cooled to ambient temperature.
1. A method for applying a diffusion barrier coating to a substrate comprising the steps of:
providing a metal substrate;
cleaning the substrate of foreign material;
coating the metal substrate with a layer of chromium containing paint, said paint comprising substantially chromium, solvents, and binders;
baking the layer of chromium containing paint to a temperature for a period of time sufficient to volatilize the solvents in the layer of chromium containing paint;
baking the layer of chromium containing paint to a second temperature for a second period of time sufficient to volatilize the binders in the layer of chromium containing paint, the remaining layer being substantially contiguous on the substrate surface and comprising substantially chromium of sufficient thickness;
heating the metal substrate and layer of chromium to a third temperature for a third period of time sufficient to diffuse the chromium into the substrate to form a diffusion chromium layer; and
cooling the substrate.
2. The method of claim 1 further comprising the step of applying an outer coating over the diffusion metal layer after cooling the substrate.
3. A low pressure turbine blade coated with a diffusion barrier using the method of claim 2 .
4. The method of claim 1 wherein the first temperature is in the range of about 300° F. to about 485° F., the first time is in the range of about one hour to about three hours, the second temperature is in the range of about 750° F. to about 930° F., the second time is in the range of about one hour to about three hours, the third temperature is in the range of about 1200° F. to about 2010° F. and the third time is in the range of about one hour to about four hours.
5. The method of claim 4 wherein the first temperature is about 400° F., the first time is about two hours, the second temperature is about 750° F. and the second time is about two hours, the third temperature is about 1830° F. and the third time is about two hours.
6. The method of claim 5 further comprising the step of applying an outer coating over the diffusion metal layer after cooling the substrate.
7. A low pressure turbine blade coated with a diffusion barrier using the method of claim 6 .
8. A high pressure turbine blade coated with a diffusion barrier using the method of claim 6 .
9. A low pressure turbine blade coated with a diffusion barrier using the method of claim 1 .
10. A high pressure turbine blade coated with a diffusion barrier using the method of claim 1 .
11. A method for applying a diffusion barrier coating to a substrate comprising the steps of:
providing a metal substrate;
cleaning the substrate of foreign material;
coating the metal substrate with a layer of chromium and aluminum alloy containing paint, wherein the percentage of the metal that is chromium is in the range of about 5 weight percent to about 25 weight percent, said paint comprising substantially chromium and aluminum alloy, solvents, and binders;
baking the layer of chromium and aluminum alloy containing paint to a temperature for a period of time sufficient to volatilize the solvents in the layer of chromium and aluminum alloy;
baking the layer of chromium and aluminum alloy containing paint to a second temperature for a second period of time sufficient to volatilize the binders in the layer of chromium and aluminum alloy containing paint, the remaining layer being substantially contiguous on the substrate surface and comprising substantially chromium and aluminum alloy of sufficient thickness;
heating the metal substrate and layer of chromium and aluminum alloy to a third temperature for a third period of time sufficient to diffuse the chromium and aluminum alloy into the substrate to form a diffusion chromium and aluminum layer; and
cooling the substrate.
12. The method of claim 11 , wherein the percentage of the alloy that is chromium is about 20 weight percent.
13. The method of claim 12 wherein the first temperature is in the range of about 300° F. to about 485° F., the first time is in the range of about one hour to about three hours, the second temperature is in the range of about 750° F. to about 930° F., the second time is in the range of about one hour to about three hours, the third temperature is in the range of about 1200° F. to about 1830° F. and the third time is in the range of about one hour to about four hours.
14. The method of claim 13 wherein the first temperature is about 400° F., the first time is about two hours, the second temperature is about 750° F. and the second time is about two hours, the third temperature is about 1600° F. and the third time is about two hours.
15. The method of claim 14 further comprising the step of applying an outer coating over the diffusion metal layer after cooling the substrate.
16. The method of claim 11 wherein the first temperature is in the range of about 300° F. to about 485° F., the first time is in the range of about one hour to about three hours, the second temperature is in the range of about 750° F. to about 930° F., the second time is in the range of about one hour to about three hours, the third temperature is in the range of about 1200° F. to about 1830° F. and the third time is in the range of about one hour to about four hours.
17. The method of claim 16 , wherein the first temperature is about 400° F., the first time is about two hours, the second temperature is about 750° F. and the second time is about two hours, the third temperature is about 1600° F. and the third time is about two hours.
18. A low pressure turbine blade coated with a diffusion barrier using the method of claim 11 .
19. A high pressure turbine blade coated with a diffusion barrier using the method of claim 11 .