首页> 外国专利> THERMAL BARRIER COATING MEMBER, METHOD FOR PRODUCING THE SAME, THERMAL BARRIER COATING MATERIAL, GAS TURBINE, AND SINTERED BODY

THERMAL BARRIER COATING MEMBER, METHOD FOR PRODUCING THE SAME, THERMAL BARRIER COATING MATERIAL, GAS TURBINE, AND SINTERED BODY

机译:热障涂层构件,其制造方法,热障涂层材料,燃气轮机和烧结体

摘要

There are provided a thermal barrier coating material and athermal barrier coating member that can suppress spalling whenused at a high temperature and have a high thermal barriereffect, a method for producing the same, a turbine membercoated with a thermal barrier coating, and a gas turbine. Thethermal barrier coating member comprises a heat resistantsubstrate 21, a bond coat layer 22 formed thereon, and aceramic layer 24 formed further thereon, wherein the ceramiclayer 24 comprises an oxide which consists of an oxiderepresented by the general formula A2Zr2O7 doped with apredetermined amount of CaO or MgO and has 10 volume % or moreof a pyrochlore type crystal structure, where A represents anyof La, Nd, Sm, Gd, and Dy.
机译:提供了一种隔热涂层材料和一种隔热涂层部件,可在出现以下情况时抑制剥落在高温下使用并具有较高的热障效果,其制造方法,涡轮构件涂有隔热涂层和燃气轮机。的隔热涂层构件包括耐热性基板21,在其上形成的粘结涂层22以及在其上进一步形成的陶瓷层24,其中陶瓷层24包括由氧化物组成的氧化物由通式A2Zr2O7掺杂预定量的CaO或MgO,并且具有10%或更多的体积烧绿石型晶体结构,其中A代表任何的La,Nd,Sm,Gd和Dy。

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