Barrier coating with calcium aluminosilicate additive
A gas turbine engine article includes a substrate and a silicate-resistant barrier coating disposed on the substrate. The silicate-resistant barrier coating is composed of a refractory matrix and a calcium aluminosilicate additive (CAS additive) dispersed in the refractory matrix.
1. A gas turbine engine article comprising:
a substrate; and
a silicate-resistant barrier coating disposed on the substrate, the silicate-resistant barrier coating being composed of a refractory matrix and a calcium aluminosilicate additive (CAS additive) dispersed in the refractory matrix, the refractory matrix being selected from hafnia, hafnium silicate, zirconium silicate, or combinations thereof, and the silicate resistant barrier coating including, by mol. %, 0.1 to 30 of the CAS additive and a remainder being the refractory matrix.
2. The article as recited in claim 1 , wherein the CAS additive includes, by mol. %, 30 to 90 of SiO 2 .
3. The article as recited in claim 1 , wherein the CAS additive includes, by mol. %, 5 to 30 of AlO 1.5 .
4. The article as recited in claim 1 , wherein the CAS additive includes, by mol. %, 10 to 50 of CaO.
5. The article as recited in claim 1 , wherein the CAS additive includes, by mol. %, 30 to 90 of SiO 2 , 5 to 30 of AlO 1.5 , and 10 to 50 of CaO.
6. The article as recited in claim 1 , wherein the CAS additive includes X 1 mol. % of SiO 2 , X 2 mol. % of CaO, and X 3 mol. % of AlO 1.5 , where X 1 is greater than X 2 and X 1 is greater than X 3 .
7. The article as recited in claim 6 , wherein the CAS additive includes, by mol. %, less than 10 of at least one of magnesium, barium, or strontium in the form of an oxide.
8. The article as recited in claim 1 , wherein the refractory matrix is hafnia.
9. The article as recited in claim 1 , wherein the silicate resistant barrier coating includes, by mol. %, 3 to 8 of the CAS additive.
10. The article as recited in claim 1 , wherein the refractory matrix is hafnium silicate.
11. The article as recited in claim 1 , wherein the refractory matrix is zirconium silicate.
12. The article as recited in claim 1 , wherein the CAS additive is in grain boundaries of the refractory matrix.
13. The article as recited in claim 1 , wherein the silicate-resistant barrier coating has a graded composition of the refractory matrix in a through-thickness direction.