A superalloy turbine blade (10) has a bond coating (92) and a thermal barrier coating (94). The bond coating (92) comprises a MCrAlY coating on the metallic substrate (90) of the superalloy turbine blade (10), an aluminide coating on the MCrAlY coating and an alumina interface layer (94) on the aluminide coating. The thermal barrier coating (96) is on the alumina interface layer (94). The aluminide coating on the MCrAlY provides more aluminium to bond the thermal barrier coating (6) onto the metallic substrate (90). <IMAGE>
申请公布号
DE69302678(T2)
申请公布日期
1996.09.26
申请号
DE1993602678T
申请日期
1993.03.03
申请人
ROLLS-ROYCE PLC, LONDON, GB
发明人
RICKERBY, DAVID STAFFORD, DUFFIELD, DERBY DE6 4DS, GB