| 摘要 |
A turbine engine component is provided which has a substrate (14), a yttria-stabilized zirconia coating (10) applied over the substrate (14), and a molten silicate resistant outer layer (20). The molten silicate resistant outer layer (20) is formed from gadolinia or gadolinia-stabilized zirconia. A method for forming the coating system of the present invention is described. |
