Environmental barrier multi-phase abradable coating
Disclosed is a multi-phase abradable coating including a ceramic matrix and a dislocator phase.
1. A multi-phase abradable coating comprising:
a ceramic matrix and a dislocator phase dispersed in the ceramic matrix,
wherein the dispersed dislocator phase comprises zircon and ZrO2,
wherein a portion of the ZrO2 is microcracked,
wherein the ZrO2 is configured such that it is formed near a surface by exposure to post combustion gases.
2. The multi-phase abradable coating of claim 1 , wherein the ceramic matrix comprises hafnium dioxide, a rare earth disilicate, a rare earth monosilicate, BSAS, hafnium silicate, or a combination thereof.
3. A coating system on a ceramic matrix composite component comprising:
a multi-phase abradable coating in combination with a top coat, a bond coat or a combination thereof,
wherein the multi-phase abradable coating comprises a ceramic matrix and a dislocator phase dispersed in the ceramic matrix,
wherein the dispersed dislocator phase comprises zircon and ZrO2,
wherein a portion of the ZrO2 is microcracked,
wherein the ZrO2 is configured such that it is formed near a surface by exposure to post combustion gases.
4. The coating system of claim 3 , wherein the ceramic matrix comprises hafnium dioxide, a rare earth disilicate or a combination thereof.
5. The coating system of claim 3 , wherein the coating system comprises the top coat and the bond coat and further wherein the bond coat is disposed on the ceramic matrix component and the top coat is disposed between the bond coat and the multi-phase abradable coating.
6. The coating system of claim 3 , wherein the coating system comprises the top coat disposed between the ceramic matrix component and the multi-phase abradable coating.
7. The coating system of claim 3 , wherein the coating system comprises the bond coat disposed between the ceramic matrix component and the multi-phase abradable coating.
8. The coating system of claim 3 , wherein the bond coat comprises silicon.
9. The coating system of claim 3 , wherein the top coat comprises hafnium dioxide, a rare earth disilicate, or a combination thereof.
10. The coating system of claim 3 , wherein the top coat and the ceramic matrix comprise the same material.
11. The coating system of claim 3 , wherein the ceramic matrix composite component is a shroud for the turbine section of a gas turbine engine.