发明名称 THERMAL BARRIER COATING MEMBER, METHOD FOR PRODUCING THE SAME, USE OF THE THERMAL BARRIER COATING MATERIAL, GAS TURBINE, AND SINTERED BODY
摘要 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.
申请公布号 EP2371987(B1) 申请公布日期 2016.12.21
申请号 EP20110171531 申请日期 2006.10.06
申请人 Mitsubishi Hitachi Power Systems, Ltd. 发明人 Namba, Katsumi;Torigoe, Taiji;Okada, Ikuo;Mori, Kazutaka;Nagano, Ichiro;Kawata, Yutaka;Takahashi, Koji
分类号 C04B35/486;C23C4/02;C23C4/11;C23C30/00;F01D5/28;F02K9/97 主分类号 C04B35/486
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