首页> 外国专利> THERMAL BARRIER COATING MEMBER, PRODUCTION METHOD THEREFOR, THERMAL BARRIER COATING MATERIAL, GAS TURBINE, AND SINTERED COMPACT

THERMAL BARRIER COATING MEMBER, PRODUCTION METHOD THEREFOR, THERMAL BARRIER COATING MATERIAL, GAS TURBINE, AND SINTERED COMPACT

机译:热障涂层成员,其生产方法,热障涂层材料,燃气轮机和烧结体

摘要

PPROBLEM TO BE SOLVED: To provide a thermal barrier coating material and a thermal barrier coating member which can be prevented from peeling when in use under high temperature and have excellent thermal barrier effect; to provide a method for production of the thermal barrier coating member; and also to provide a turbine member coated with the thermal barrier coating material, and a gas turbine. PSOLUTION: The thermal barrier coating member includes a heat-resistant base material 21, a bond coat layer 22 formed on the heat-resistant base material, and a ceramic layer 24 formed on the bond coat layer. The ceramic layer 24 contains oxides expressed by general formula: A"SB2/SBCeSB2/SBOSB7/SB, wherein A" is any one of La, Sm or Yb. PCOPYRIGHT: (C)2011,JPO&INPIT
机译:

要解决的问题:提供一种隔热涂层材料和隔热涂层构件,其在高温下使用时可以防止剥离并且具有优异的隔热效果;提供一种生产隔热涂层构件的方法;并且还提供涂覆有隔热涂层材料的涡轮构件和燃气涡轮。

解决方案:隔热涂层构件包括耐热基材21,在耐热基材上形成的粘结涂层22和在粘结涂层上形成的陶瓷层24。陶瓷层24包含由通式A” 2 Ce 2 O 7 表示的氧化物,其中A”是La,Sm中的任何一种。或Yb。

版权:(C)2011,日本特许厅&INPIT

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