发明名称 HEAT-RESISTANT MEMBER, AND GAS TURBINE HOT PART
摘要 PROBLEM TO BE SOLVED: To provide a heat-resistant member such as a gas turbine hot part which has durability and reliability in the use under a corrosive environment with the use of the low-grade oil.SOLUTION: The heat resistant member includes an alloy substrate containing Ni, Co, or Fe as a principal component, and thermal barrier coating formed on the surface of the substrate via a bonding layer. The thermal barrier coating includes a porous thermal-barrier layer made of ceramic and an environmental barrier layer with corrosion resistance. An impregnated layer is provided between the environmental barrier layer and the thermal barrier layer. In the impregnated layer, the thermal barrier layer is impregnated with a part of the environmental barrier layer. In particular, the thermal barrier layer is made of a porous zirconia layer, and the environmental barrier layer includes silica as a principal component. The porous zirconia layer has pores impregnated with the part of the environmental barrier layer. As a result, the heat resistant member having excellent corrosion resistance and excellent heat resistance are attained.
申请公布号 JP2011012287(A) 申请公布日期 2011.01.20
申请号 JP20090154526 申请日期 2009.06.30
申请人 HITACHI LTD 发明人 ARIKAWA HIDEYUKI;MEHATA TERU;KOJIMA YOSHIYUKI;ICHIKAWA KUNIHIRO;HARUYAMA HIROSHI
分类号 C23C4/18;C23C4/06;C23C4/10;F01D5/28;F02C7/00;F23R3/42 主分类号 C23C4/18
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