发明名称 |
THERMAL BARRIER COATING FOR GAS TURBINE ENGINE COMPONENTS |
摘要 |
A component for a gas turbine engine according to an exemplary embodiment of the present disclosure can include a substrate, a thermal barrier coating deposited on at least a portion of the substrate, and an outer layer deposited on at least a portion of the thermal barrier coating. The outer layer can include a material that is reactive with an environmental contaminant that comes into contact with the outer layer to alter a microstructure of the outer layer. |
申请公布号 |
EP2893148(A4) |
申请公布日期 |
2015.11.04 |
申请号 |
EP20130849810 |
申请日期 |
2013.08.08 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
SHROCK, CHRISTOPHER W.;MALONEY, MICHAEL;LITTON, DAVID A.;ZIMMERMAN, BENJAMIN JOSEPH;HAZEL, BRIAN T. |
分类号 |
F01D5/18;C23C4/02;C23C4/08;C23C4/10;C23C4/12;C23C28/00;F01D5/14;F02C7/00 |
主分类号 |
F01D5/18 |
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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