发明名称 Thermal barrier coating memner and method of producing the same
摘要 A thermal barrier coating member to be used for such as a member for a gas turbine comprising a metallic member comprising a super alloy mainly composed of at least one of Ni, Co and Fe, an intermediate layer composed of a MCrAlY alloy (M denotes at least one of Ni, Co and Fe) covering this metallic substrate, and a ceramic layer mainly composed of stabilized zirconia formed on the intermediate layer. A ceramic material having a higher melting point than zirconia is compounded in the ceramic layer as a member for suppressing a reaction sintering of the ceramic layer.
申请公布号 GB2317400(B) 申请公布日期 1999.02.24
申请号 GB19970020025 申请日期 1997.09.19
申请人 KABUSHIKI KAISHA * TOSHIBA 发明人 TAKAHIRO * HAMADA;MASASHI * TAKAHASHI;MASAHIRO * SAITOH;YOSHIYASU * ITOH
分类号 C23C28/00;C23C4/02;C23C16/04;C23C16/32;C23C16/34;C23C16/38;C23C16/40;C23C16/44;(IPC1-7):C23C4/10;C23C4/18;C23C16/30 主分类号 C23C28/00
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