发明名称 THERMAL BARRIER COATING MATERIAL, METHOD OF PRODUCTION THEREOF, AND GAS TURBINE MEMBER AND GAS TURBINE APPLYING THE THERMAL BARRIER COATING MATERIAL
摘要 <p>Disclosed is a thermal barrier coating (TBC) raw material for coating a gas turbine member that provides a higher thermal barrier property and a higher peeling resistance. The thermal barrier coating (TBC) raw material comprises a zirconia powder having a specific surface area of at least 10 m2/g and a rare earth oxide having a specific surface area of at least 10 m2/g.</p>
申请公布号 CA2669781(C) 申请公布日期 2010.10.05
申请号 CA20022669781 申请日期 2002.06.14
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 TORIGOE, TAIJI;MORI, KAZUTAKA;OKADA, IKUO;AOKI, SUNAO;TAKAHASHI, KOUJI;OHARA, MINORU;HIRATA, TAKEHIKO;KANEKO, HIDEAKI
分类号 C23C4/10;C23C4/08;C23C4/18;C23C28/00;F01D5/28 主分类号 C23C4/10
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