发明名称 Ceramic thermal barrier coating with alumina interlayer
摘要 A ceramic thermal barrier coating system for superalloy components subjected to high operating temperatures, such as gas turbine engine airfoils, includes a high purity alumina interfacial layer between the metallic substrate and the ceramic overcoat in order to better resist failure by spalling.
申请公布号 US5015502(A) 申请公布日期 1991.05.14
申请号 US19890433886 申请日期 1989.11.08
申请人 ALLIED-SIGNAL INC. 发明人 STRANGMAN, THOMAS E.;SOLFEST, PATRICIA A.
分类号 C23C14/08;C23C14/16;C23C16/40;F01D5/28 主分类号 C23C14/08
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