发明名称 Gas turbine engine and method of producing the same
摘要 A raw material powder having particle sizes of not more than 125 mum and preferably not more than 75 mum, such as a powder of an alloy of Co-32% Ni-21% Cr-7.5% Al-0.5% Y is thermally sprayed onto surfaces of shroud members of a shroud to form a coating. The high velocity oxygen-fuel thermal spray method is used as the thermal spray method. In the obtained coating, the porosity is 5% to 30% by volume and the oxygen content is not more than 2% by weight. In particular, when the raw material powder has particle sizes of about 40 mum, it is possible to obtain the coating which has an extremely small oxygen content of about 0.5% by weight.
申请公布号 US7163370(B2) 申请公布日期 2007.01.16
申请号 US20040763375 申请日期 2004.01.23
申请人 HONDA MOTOR CO., LTD. 发明人 KOKUSHO TSUYOSHI
分类号 F01D11/00;F01D11/12;C23C4/00;C23C4/02;C23C4/06;C23C4/08;C23C4/12;F01D5/28;F01D25/00 主分类号 F01D11/00
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