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THERMAL BARRIER COATING MATERIAL, METHOD OF PRODUCTION THEREOF, AND GAS TURBINE MEMBER AND GAS TUR 发明授权

2023-12-11 2640 2880K 0

专利信息

申请日期 2025-07-27 申请号 CA2451495
公开(公告)号 CA2451495C 公开(公告)日 2010-07-27
公开国别 CA 申请人省市代码 全国
申请人 MITSUBISHI HEAVY INDUSTRIES LTD
简介 A thermal barrier coating material, characterized in that it comprises a metal binder layer (22) and a porous ceramic layer (23) comprising a partially stabilized ZrO2which are laminated on a base material (2) in this order, and the ceramic layer has microcracks (24) extending in the thickness direction; and a method for producing the thermal barrier coating material which comprises, after the lamination of the ceramic layer, heating the front surface of the ceramic layer by the irradiation with a laser beam while cooling the back face of the base material, to thereby form the microcraks. Another thermal barrier coating material, characterized in that it comprises a metal binder layer and, laminated thereon, a partially stabilized ZrO2 which is partially stabilized by the addition of Dy2O2 and Yb2O2. A thermal spray material for TBC, characterized in that it comprises a zirconia powder and a rare earth oxide powder added thereto, both having a specific surface area of 10 m2/g; and a method for producing the thermal spray material which comprises mixing these powders and a binder to form a slurry, granulating the slurry, and heat-treating the resultant granules.


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