发明名称 |
THERMAL BARRIER COATING MEMBER, PRODUCTION METHOD THEREFOR, THERMAL BARRIER COATING MATERIAL, GAS TURBINE, AND SINTERED COMPACT |
摘要 |
<P>PROBLEM TO BE SOLVED: To provide a thermal barrier coating material and a thermal barrier coating member which can be prevented from peeling when in use under high temperature and have excellent thermal barrier effect; to provide a method for production of the thermal barrier coating member; and also to provide a turbine member coated with the thermal barrier coating material, and a gas turbine. <P>SOLUTION: The thermal barrier coating member includes a heat-resistant base material 21, a bond coat layer 22 formed on the heat-resistant base material, and a ceramic layer 24 formed on the bond coat layer. The ceramic layer 24 contains oxides expressed by general formula: A"<SB>2</SB>Ce<SB>2</SB>O<SB>7</SB>, wherein A" is any one of La, Sm or Yb. <P>COPYRIGHT: (C)2011,JPO&INPIT |
申请公布号 |
JP2010242223(A) |
申请公布日期 |
2010.10.28 |
申请号 |
JP20100160679 |
申请日期 |
2010.07.15 |
申请人 |
MITSUBISHI HEAVY IND LTD |
发明人 |
NANBA KATSUMI;TORIGOE TAIJI;OKADA IKUO;MORI KAZUTAKA;NAGANO ICHIRO;KAWADA YUTAKA;TAKAHASHI KOJI |
分类号 |
C23C4/10;C23C4/08;C23C14/08 |
主分类号 |
C23C4/10 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|