Coating structure, turbine part having same, and method for manufacturing coating structure
Provided are a coating structure, a turbine part having the same, and a method for manufacturing the coating structure. The coating structure is provided on a surface of a base portion including a ceramic matrix composite. The coating structure is layered on the surface of the base portion, and includes a bond coat layer formed of a rare-earth silicate and a top coat layer layered on the bond coat layer. The residual stress present in the bond coat layer is compressive residual stress. The oxygen permeability coefficient of the bond coat layer is no greater than 10 −9 kg·m −1 ·s −1 at a temperature of not lower than 1200° C. and a higher oxygen partial pressure of not less than 0.02 MPa. The bond coat layer may contain carbonitride particles or carbonitride whiskers.
1. A coating structure provided on a surface of a base portion including a ceramic matrix composite comprising:
a bond coat layer formed of a rare-earth silicate, the bond coat layer layered on the surface of the base portion; and
a top coat layer layered on the bond coat layer,
wherein the bond coat layer has a compressive residue stress as a residual stress, and an oxygen permeability coefficient of not greater than 10 −9 Kg·m −1 ·s −1 at not lower than 1200° C. and a higher oxygen partial pressure of not less than 0.02 MPa, and
wherein the top coat layer has tensile residual stress.
2. The coating structure according to claim 1 , wherein the bond coat layer has a crystal ratio of from 90% to 100%.
3. The coating structure according to claim 1 , wherein the bond coat layer is layered without another material interposed between the bond coat layer and the surface of the base portion.
4. The coating structure according to claim 1 , wherein the residue stress of the bond coat layer is smaller than that of the top coat layer.
5. The coating structure according to claim 1 , wherein the bond coat layer has a grain size of from 0.01 μm to 10 μm.
6. The coating structure according to claim 1 , wherein in the rare-earth silicate of the bond coat layer, a dispersed material containing silicon or titanium is dispersed.
7. The coating structure according to claim 6 , wherein the dispersed material is particles.
8. The coating structure according to claim 6 , wherein the dispersed material is whiskers.
9. The coating structure according to claim 6 , wherein the dispersed material contains nitrogen.
10. A turbine part comprising the coating structure according to claim 1 and the base portion including the coating structure on the surface.