发明名称 THERMAL BARRIER COATING MATERIAL, THERMAL BARRIER COATING, TURBINE MEMBER, AND GAS TURBINE
摘要 <p>A thermal barrier coating material that exhibits superior high-temperature crystal stability to YSZ, as well as a high degree of toughness and an excellent thermal barrier effect. Also provided are a thermal barrier coating, which has a ceramic layer formed using the thermal barrier coating material and exhibits excellent durability to heat cycling, and a turbine member and a gas turbine which are each provided with the thermal barrier coating. The thermal barrier coating material comprises mainly ZrO 2 which contains Yb 2 O 3 and Sm 2 O 3 as stabilizers, wherein the amount of the stabilizers is not less than 2 mol% and not more than 7 mol%, and the amount of the Sm 2 O 3 is not less than 0.1 mol% and not more than 2.5 mol%.</p>
申请公布号 KR20110066186(A) 申请公布日期 2011.06.16
申请号 KR20117008968 申请日期 2009.11.27
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 TORIGOE TAIJI;NAGANO ICHIRO;OKADA IKUO;TSUKAGOSHI KEIZO;TAKAHASHI KOJI;OKAJIMA YOSHIFUMI;KASUMI SOJI;ITO EISAKU;MORI KAZUTAKA
分类号 C23C26/00;C23C4/10;F01D5/28 主分类号 C23C26/00
代理机构 代理人
主权项
地址