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
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