发明名称 |
HIGH TEMPERATURE RESISTANT MEMBER AND GAS TURBINE |
摘要 |
PROBLEM TO BE SOLVED: To maintain CMAS resistance stably for a long period of time.SOLUTION: A high temperature resistant member 10 includes: a heat resistant alloy base material 21; and a porous ceramic layer 23 for cladding the base material 21, in which a number of pores 23a are formed. The high temperature resistant member further includes a composite oxide impregnation part 25 impregnated with a composite oxide 26 containing Zr as a metal element, at least on a surface side in the porous ceramic layer 23. |
申请公布号 |
JP2013136845(A) |
申请公布日期 |
2013.07.11 |
申请号 |
JP20130056976 |
申请日期 |
2013.03.19 |
申请人 |
MITSUBISHI HEAVY IND LTD |
发明人 |
NAGANO ICHIRO;TORIGOE TAIJI;MORI KAZUTAKA;OKAJIMA YOSHIFUMI;KAMIMURA YOSHIHISA |
分类号 |
C23C4/10;C23C4/08;C23C4/18;F01D5/28;F02C7/00;F23R3/42 |
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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