Low porosity abradable coating
An article for use in a high-temperature environment that includes a substrate including a superalloy material, a ceramic, or a ceramic matrix composite, and an abradable coating on the substrate, the abradable coating including a rare earth silicate and a dislocator phase, the dislocator phase forms one or more distinct phase regions in the abradable coating and comprises at least one of hafnium diboride (HfB 2 ), zirconium diboride (ZrB 2 ), tantalum nitride (TaN or Ta 2 N), tantalum carbide (Ta 2 C), titanium diboride (TiB 2 ), zirconium carbide (ZrC), hafnium carbide (HfC), tantalum diboride (TaB 2 ), hafnium nitride (HfN), or niobium carbide (NbC).
1. An article for use in a high-temperature environment comprising:
a substrate comprising a superalloy material, a ceramic, or a ceramic matrix composite; and
an abradable coating on the substrate, the abradable coating comprising a rare earth silicate and a dislocator phase, wherein the dislocator phase forms one or more distinct phase regions in the abradable coating and comprises at least one of hafnium diboride (HfB 2 ), zirconium diboride (ZrB 2 ), tantalum nitride (TaN or Ta 2 N), tantalum carbide (Ta 2 C), titanium diboride (TiB 2 ), zirconium carbide (ZrC), hafnium carbide (HfC), tantalum diboride (TaB 2 ), hafnium nitride (HfN), or niobium carbide (NbC), and wherein the abradable coating comprises between about 5 percent by weight (wt. %) and about 20 wt. % of the dislocator phase.
2. The article of claim 1 , wherein the dislocator phase reduces the internal mechanical strength of the abradable coating.
3. The article of claim 2 , wherein the abradable coating further comprises at least one additive selected from the group consisting of calcium oxide (CaO), barium oxide (BaO), magnesium oxide (MgO), titanium dioxide (TiO 2 ), alumina (Al 2 O 3 ), silicon dioxide (SiO 2 ), tantalum pentoxide (Ta 2 O 5 ), hafnium silicate (HfSiO 4 ), an alkali oxide, and an alkali earth oxide.
4. The article of claim 1 , wherein the dislocator phase has a lower coefficient of friction than the rare earth silicate.
5. The article of claim 1 , wherein the abradable coating defines a porosity of less than 20 percent by volume (vol. %).
6. The article of claim 1 , wherein the rare earth silicate comprises at least one of ytterbium monosilicate or ytterbium disilicate.
7. The article of claim 1 , further comprising:
a bond coat on the substrate; and
an environmental barrier coating (EBC) or a thermal barrier coating (TBC) between the bond coat and the abradable coating.
8. The article of claim 7 , wherein the article comprises the EBC, wherein the EBC comprises:
a base layer on the bond coat, the base layer comprising a first rare earth silicate; and
a barrier coating on the base layer, the barrier coating comprising a first layer and a second layer on the first layer, the first layer comprising barium-strontium-aluminosilicate, the second layer comprising a second rare earth silicate.
9. The article of claim 8 , wherein the second layer further comprises at least one dopant selected from the group consisting of alumina, an alkali oxide, an alkaline earth oxide, and combinations thereof.
10. The article of claim 7 , wherein the article comprises the EBC, wherein the EBC comprises:
a base layer on the bond coat, the base layer comprising a first rare earth silicate; and
a barrier coating on the bond coat, the barrier coating comprising a second rare earth silicate and at least one of TiSi 2 or MoSi 2 .
11. The article of claim 7 , wherein the EBC or the TBC comprises a calcium-magnesium-alumino-silicate (CMAS) resistant layer, wherein the CMAS-resistant layer comprises a rare earth silicate and at least one additive selected from the group consisting of calcium oxide (CaO), barium oxide (BaO), magnesium oxide (MgO), titanium dioxide (TiO 2 ), alumina (Al 2 O 3 ), silicon dioxide (SiO 2 ), tantalum pentoxide (Ta 2 O 5 ), hafnium silicate (HfSiO 4 ), an alkali oxide, an alkali earth oxide, and combinations thereof.
12. A method comprising:
depositing a bond coat on a substrate, wherein the substrate comprises a superalloy material, a ceramic, or a ceramic matrix composite;
depositing an environmental barrier coating (EBC) or a thermal barrier coating (TBC) on the bond coat;
depositing an abradable coating on the EBC or the TBC wherein the abradable coating comprises a rare earth silicate and a dislocator phase, wherein the dislocator phase forms one or more distinct phase regions in the abradable coating and comprises at least one of hafnium diboride (HfB 2 ), zirconium diboride (ZrB 2 ), tantalum nitride (TaN or Ta 2 N), tantalum carbide (Ta 2 C), titanium diboride (TiB 2 ), zirconium carbide (ZrC), hafnium carbide (HfC), tantalum diboride (TaB 2 ), hafnium nitride (HfN), or niobium carbide (NbC) wherein depositing the EBC or the TBC comprises:
depositing a base layer on the bond coat, the base layer comprising a first rare earth silicate; and
depositing a barrier coating on the base layer, wherein depositing the barrier coating on the base layer comprises at least one of:
depositing a first layer comprising barium-strontium-aluminosilicate and a second layer comprising a second rare earth silicate, or
depositing a layer comprising a second rare earth silicate and at least one of TiSi 2 or MoSi 2 .
13. The method of claim 12 , wherein the dislocator phase reduces the internal mechanical strength of the abradable coating.
14. The method of claim 13 , wherein the abradable coating further comprises at least one additive selected from the group consisting of calcium oxide (CaO), barium oxide (BaO), magnesium oxide (MgO), titanium dioxide (TiO 2 ), alumina (Al 2 O 3 ), silicon dioxide (SiO 2 ), tantalum pentoxide (Ta 2 O 5 ), hafnium silicate (HfSiO 4 ), an alkali oxide, and an alkali earth oxide.
15. The method of claim 12 , wherein depositing the abradable coating on the EBC or the TBC comprises depositing a mixture of particles using suspension thermal spraying or thermal spraying, wherein the mixture of particles comprises a first plurality of particles comprising the rare earth silicate, and a second plurality of particles comprising the dislocator phase.
16. The method of claim 15 , wherein the mixture of particles further comprises the rare earth silicate and the at least one additive.
17. The method of claim 12 , wherein the abradable coating defines a porosity of less than 20 percent by volume (vol. %).
18. An article for use in a high-temperature environment, the article comprising:
a substrate comprising a superalloy material, a ceramic, or a ceramic matrix composite; and
an abradable coating on the substrate, the abradable coating comprising a rare earth silicate and a dislocator phase, wherein the dislocator phase forms one or more distinct phase regions in the abradable coating and comprises at least one of hafnium diboride (HfB 2 ), zirconium diboride (ZrB 2 ), tantalum nitride (TaN or Ta 2 N), tantalum carbide (Ta 2 C), titanium diboride (TiB 2 ), zirconium carbide (ZrC), hafnium carbide (HfC), tantalum diboride (TaB 2 ), hafnium nitride (HfN), or niobium carbide (NbC), and wherein the abradable coating defines a porosity of less than 20 percent by volume (vol. %).
19. The article of claim 18 , wherein the abradable coating further comprises at least one additive selected from the group consisting of calcium oxide (CaO), barium oxide (BaO), magnesium oxide (MgO), titanium dioxide (TiO 2 ), alumina (Al 2 O 3 ), silicon dioxide (SiO 2 ), tantalum pentoxide (Ta 2 O 5 ), hafnium silicate (HfSiO 4 ), an alkali oxide, and an alkali earth oxide.
20. The article of claim 1 , wherein the rare earth silicate comprises at least one of ytterbium monosilicate or ytterbium disilicate.