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
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