发明名称 Laser segmented thick thermal barrier coatings for turbine shrouds
摘要 A turbine shroud having a coating comprising a bond layer covering the shroud substrate, and a thick ceramic stabilized zirconia layer with a segmented morphology covering the bond coat. The segmented morphology is defined by an array of slots or grooves which extend from the outer surface of the ceramic layer inwards through almost the entire thickness of the coating but without piercing the underlying substrate. The segmented morphology comprises a plurality of grooves that are laser drilled into the ceramic layer. Each groove is formed by laser drilling a series of holes that are spaced from each other so that the groove has a fully segmented portion and a partially segmented portion.
申请公布号 US6224963(B1) 申请公布日期 2001.05.01
申请号 US19980067257 申请日期 1998.04.27
申请人 ALLIEDSIGNAL INC. 发明人 STRANGMAN THOMAS E.
分类号 F02C7/00;B32B18/00;C23C4/18;C23C28/00;F01D11/12;(IPC1-7):B32B3/00;C03C27/02 主分类号 F02C7/00
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