发明名称 |
COMPOSITION DE BARRIERE THERMIQUE DE FAIBLE CONDUCTIVITE THERMIQUE, PIECE MECANIQUE EN SUPERALLIAGE PROTEGEE PAR UN REVETEMENT DE CERAMIQUE AYANT UNE TELLE COMPOSITION, ET METHODE DE REALISATION DU REVETEMENT DE CERAMIQUE |
摘要 |
<p>Thermal barrier composition is based on zirconia containing dysprosium oxide for stabilization and thermal conductivity reduction. A low thermal conductivity thermal barrier composition is based on zirconia containing dysprosium oxide, for stabilization and thermal conductivity reduction, and optionally an oxide of a tetravalent metal of atomic weight greater than that of zirconium. Independent claims are also included for: (i) a mechanical part of a superalloy having a ceramic coating of the above composition; and (ii) a method of forming a thermal barrier coating on a superalloy substrate by depositing the above composition on a bond layer on the substrate.</p> |
申请公布号 |
FR2798654(B1) |
申请公布日期 |
2001.10.19 |
申请号 |
FR19990011565 |
申请日期 |
1999.09.16 |
申请人 |
SOCIETE NATIONALE D&apos,ETUDE ET DE CONSTRUCTION DE MOTEURS D&apos,AVIATION SNECMA |
发明人 |
ALPERINE SERGE ALEXANDRE;ARNAULT VERONIQUE;LAVIGNE ODILE;MEVREL REMY |
分类号 |
C04B35/48;C23C4/02;C23C14/08;C23C28/00;C23C30/00;(IPC1-7):C04B35/48 |
主分类号 |
C04B35/48 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|