Composite coating layer for ceramic matrix composite substrate
An article may include a substrate including a ceramic matrix composite (CMC); a composite coating layer including a first coating material that includes a rare-earth disilicate and a second coating material that includes at least one of a rare-earth monosilicate, a CMAS-resistant material, or a high-temperature dislocating material, where the second coating material forms a substantially continuous phase in the composite coating layer.
1. An article comprising:
a substrate including a ceramic matrix composite (CMC);
a single composite coating layer formed from a composite feedstock, the composite feedstock comprising:
a first coating material comprising a rare-earth disilicate; and
a second coating material comprising at least one of a calcium-magnesium-alumino-silicate (CMAS)-resistant material or a high-temperature dislocating material,
wherein the second coating material forms a substantially continuous phase in the single composite coating layer, and wherein the single composite coating layer comprises splats of the first coating material evenly distributed throughout the substantially continuous phase of the second coating material and substantially fully encapsulated by the second coating material.
2. The article of claim 1 , wherein the second coating material comprises the CMAS-resistant material, and wherein the CMAS-resistant material comprises at least one of a rare-earth zirconate, a rare-earth oxide, calcia, alumina, or silica.
3. The article of claim 1 , wherein the second coating material comprises the high-temperature dislocating material, and wherein the high-temperature dislocating material comprises at least one of hafnium diboride, zirconium diboride, tantalum nitride, or tantalum carbide.
4. The article of claim 1 , wherein the single composite coating layer is substantially dense having a porosity of less than about 10 vol. %.
5. The article of claim 1 , wherein the single composite coating layer is a porous abradable coating having a porosity of greater than about 10 vol. %.
6. The article of claim 1 , further comprising an environmental barrier coating, wherein the environmental barrier coating is between the substrate and the single composite coating layer.
7. The article of claim 1 , further comprising an overlayer on the single composite coating layer, wherein the single composite coating layer is a compositional transition layer between one of the substrate, a bond coat, or an environmental barrier coating and the overlayer.
8. The article of claim 1 , wherein the single composite coating layer comprises about 5 vol. % to about 50 vol. % of the second coating material.
9. A composite feedstock comprising:
a core comprising a first coating material comprising a rare-earth disilicate; and
an outer layer at least partially encapsulating the core, wherein the outer layer comprises a second coating material comprising at least one of a rare-earth monosilicate, a CMAS-resistant material, or a high-temperature dislocating material, wherein the second coating material at least partially encapsulates respective surfaces of the core.
10. The composite feedstock of claim 9 , wherein the second coating material comprises the CMAS-resistant material, and wherein the CMAS-resistant material comprises at least one of a rare-earth zirconate, a rare-earth oxide, calcia, alumina, or silica.
11. The composite feedstock of claim 9 , wherein the second coating material comprises the high-temperature dislocating material, and wherein the high-temperature dislocating material comprises at least one of hafnium diboride, zirconium diboride, tantalum nitride, or tantalum carbide.
12. The composite feedstock of claim 9 , wherein the composite feedstock is formed by at least one of a physical blending, a sol-gel process, chemical vapor deposition, a cladding process, or refractory precursor coating.
13. An article comprising:
a substrate including a ceramic matrix composite (CMC);
a single composite coating layer comprising:
a first coating material comprising a rare-earth disilicate; and
a second coating material comprising at least one of a calcium-magnesium-alumino-silicate (CMAS)-resistant material or a high-temperature dislocating material,
wherein the second coating material forms a substantially continuous phase in the single composite coating layer, and wherein the single composite coating layer comprises splats of the first coating material evenly distributed throughout the substantially continuous phase of the second coating material and substantially fully encapsulated by the second coating material.