发明名称 |
Method for forming thermal barrier coating on hot-gas-path components of gas turbine during operation |
摘要 |
Disclosed is a method for formation of a thermal bather coating on a gas turbine during operation thereof, which includes addition of an organic compound containing silicon to a fuel under a first condition in order to form a base layer on the surface of a part coming into contact with a combustion gas of the fuel in the gas turbine during operation thereof, as well as addition of the organic compound containing silicon to the fuel under a second condition in order to form a porous layer having more pores than the base layer above the base layer.
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申请公布号 |
US8449941(B2) |
申请公布日期 |
2013.05.28 |
申请号 |
US20090616128 |
申请日期 |
2009.11.10 |
申请人 |
KIM MIN TAE;KIM DOO SOO;OH WON YOUNG;KOREA ELECTRIC POWER CORPORATION;KOREA SOUTHERN POWER CO., LTD |
发明人 |
KIM MIN TAE;KIM DOO SOO;OH WON YOUNG |
分类号 |
C23C16/00 |
主分类号 |
C23C16/00 |
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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