发明名称 |
HEAT SHIELD COATING MEMBER, PROCESS FOR PRODUCING THE SAME, HEAT SHIELD COAT MATERIAL, GAS TURBINE AND SINTERED BODY |
摘要 |
<p>There are provided a thermal barrier coating material and a thermal barrier coating member that can suppress spalling when used at a high temperature and have a high thermal barrier effect, a method for producing the same, a turbine member coated with a thermal barrier coating, and a gas turbine. The thermal barrier coating member comprises a heat resistant substrate 21, a bond coat layer 22 formed thereon, and a ceramic layer 24 formed further thereon, wherein the ceramic layer 24 comprises an oxide which consists of an oxide represented by the general formula A 2 Zr 2 O 7 doped with a predetermined amount of CaO or MgO and has 10 volume % or more of a pyrochlore type crystal structure, where A represents any of La, Nd, Sm, Gd, and Dy.</p> |
申请公布号 |
EP2009131(A1) |
申请公布日期 |
2008.12.31 |
申请号 |
EP20060811394 |
申请日期 |
2006.10.06 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
NAMBA, KATSUMI;TORIGOE, TAIJI;OKADA, IKUO;MORI, KAZUTAKA;NAGANO, ICHIRO;KAWATA, YUTAKA;TAKAHASHI, KOJI |
分类号 |
C23C4/10;C04B35/48;C04B35/50;C23C14/08 |
主分类号 |
C23C4/10 |
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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