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A composition comprising a particulate corrosion resistant component, and a glass-forming binder component. The particulate corrosion resistant component comprises from 0 to about 95% alumina particulates, and from about 5 to 100% corrosion resistant non-alumina particulates having a CTE greater tha

A composition comprising a particulate corrosion resistant component, and a glass-forming binder component. The particulate corrosion resistant component comprises from 0 to about 95% alumina particulates, and from about 5 to 100% corrosion resistant non-alumina particulates having a CTE greater than that of the alumina particulates. Also disclosed is an article comprising a turbine component comprising a metal substrate and a corrosion resistant coating having thickness up to about 10 mils (254 microns) overlaying the metal substrate. At least the layer of this coating adjacent to the metal substrate comprises a glass-forming binder component and the particulate corrosion resistant component adhered to the glass-forming binder component. Further disclosed is a method comprising the following steps: (a) providing a turbine component comprising the metal substrate; (b) depositing on the metal substrate a corrosion resistant coating composition; and (c) curing the deposited corrosion resistant coating composition to form at least one layer of a corrosion resistant coating having a thickness up to about 10 mils (254 microns).

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What is claimed is: 1. A composition comprising: a particulate corrosion resistant component consisting essentially of: from 0 to about 95% alumina particulates; and from about 5 to about 100% corrosion resistant non-alumina particulates having a CTE greater that of the alumina particulates, wherei

What is claimed is: 1. A composition comprising: a particulate corrosion resistant component consisting essentially of: from 0 to about 95% alumina particulates; and from about 5 to about 100% corrosion resistant non-alumina particulates having a CTE greater that of the alumina particulates, wherein the non-alumina particulates comprise an overlay metal alloy having the formula MCrAlY, wherein M is a nickel or nickel-cobalt alloy, and wherein the corrosion resistant non-aluminum particulates further comprise yttria-stabilized zirconia; and a glass-forming phosphate-containing binder component. 2. The composition of claim 1 wherein the particulate corrosion resistant component comprises from 0 to about 50% alumina particulates; and from about 50 to a 100 non-alumina corrosion resistant particulates. 3. The composition of claim 1 wherein the phosphate-containing binder component comprises one or more of an aluminum phosphate, a magnesium phosphate, or a chromium phosphate. 4. The composition of claim 1 wherein the phosphate-containing binder component is substantially chromate free. 5. The composition of claim 4 which further comprises a liquid carrier component. 6. The composition of claim 5 wherein the liquid carrier component comprises water. 7. The composition of claim 1 wherein the particulate corrosion resistant component comprises from 0 to about 75% alumina particulates and from about 25 to 100% corrosion resistant non-alumina particulates. 8. An article comprising: a turbine component comprising a metal substrate; and a corrosion resistant coating having thickness up to about 10 mils overlaying the metal substrate, wherein at least the layer of the corrosion resistant coating adjacent to the metal substrate comprises: a glass-forming phosphate-containing binder component; and a particulate corrosion resistant component adhered to the glass-forming binder component and comprising: from 0 to about 95% alumina particulates; and from about 5 to 100% corrosion resistant non-alumina particulates having a CTE greater than that of the alumina particulates, wherein the non-alumina particulates comprise an overlay metal alloy having the formula MCrAlY, wherein M is a nickel or nickel-cobalt alloy, and wherein the corrosion resistant non-aluminum particulates further comprise yttria-stabilized zirconia. 9. The article of claim 8 wherein the turbine component is a turbine disk, a turbine shaft, or a turbine seal. 10. The article of claim 8 wherein the turbine component is a turbine blade or turbine vane. 11. The article of claim 8 wherein the corrosion resistant coating comprises a single layer. 12. The article of claim 8 wherein the corrosion resistant coating has a thickness of from about 0.1 to about 5 mils. 13. The article of claim 8 wherein the corrosion resistant coating comprises a plurality of layers, and wherein the layer adjacent to the metal substrate is an inner layer and wherein the layer overlaying and adjacent to the inner layer comprises a particulate component having a percent weight level of alumina particulates greater that of the particulate component of the inner layer or is a glassy outer sealant layer that is substantially free of particulates. 14. The article of claim 13 wherein the inner layer has a thickness of from about 0.3 to about 5 mils and wherein the layer overlaying the inner layer has a thickness of from about 0.1 to about 5 mils. 15. The article of claim 8 wherein the particulate corrosion resistant component comprises from 0 to about 50% alumina particulates and from about 50 to 100% corrosion resistant non-alumina particulates. 16. The article of claim 15 wherein the particulate component consists essentially of corrosion resistant non-alumina particulates. 17. The article of claim 8 wherein the at least one layer of the corrosion resistant coating is on a selected portion of the metal substrate. 18. An article comprising a corrosion resistant coating having at least a layer comprising: a glass-forming phosphate-containing binder component; and a particulate corrosion resistant component adhered to the glass-forming binder component and comprising: from 0 to about 95% alumina p articulates; and from about 5 to 100% corrosion resistant non-alumina particulates having a CTE greater than that of the alumina particulates, wherein the non-alumina particulates comprise an overlay metal alloy having the formula MCrAlY, wherein M is a nickel or nickel-cobalt alloy, and wherein the corrosion resistant non-aluminum particulates further comprise yttria-stabilized zirconia. 19. The article of claim 18 wherein the corrosion resistant coating comprises a single layer. 20. The article of claim 18 wherein the corrosion resistant coating has a thickness up to about 10 mils. 21. The article of claim 18 wherein the corrosion resistant coating has a thickness of from about 0.1 to about 5 mils. 22. The article of claim 18 wherein the corrosion resistant coating comprises a plurality of layers, including an inner layer and wherein the layer overlaying and adjacent to the inner layer comprises a particulate component having a percent weight level of alumina particulates greater than that of the particulate component of the inner layer or is a glassy outer sealant layer that is substantially free of p articulates. 23. The article of claim 22 wherein the inner layer has a thickness of from about 0.3 to about 5 mils and wherein the layer overlaying the inner layer has a thickness of from about 0.1 to about 5 mils. 24. The article of claim 18 wherein the particulate corrosion resistant component comprises from 0 to about 50% alumina particulates and from about 50 to 100% corrosion resistant non-alumina particulates. 25. The article of claim 18 wherein the particulate component consists essentially of corrosion resistant non-alumina particulates.