发明名称 |
LOCALIZED TRANSITIONAL COATING OF TURBINE COMPONENTS |
摘要 |
<p>Different thermal barrier coatings are deposited on different regions of the surface of a component. A first thermal barrier coating comprising an erosion resistant yttria stabilized zirconia material is deposited on a first region of the surface of the component. A second thermal barrier coating comprising an oxidation and corrosion resistant gadolinia stabilized zirconia is deposited on a second region of the surface of the component.</p> |
申请公布号 |
WO2014022285(A1) |
申请公布日期 |
2014.02.06 |
申请号 |
WO2013US52514 |
申请日期 |
2013.07.29 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
TRYON, BRIAN S.;LITTON, DAVID A. |
分类号 |
B32B15/04;F03B3/12 |
主分类号 |
B32B15/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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