发明名称 SEGMENTED THERMALLY INSULATING COATING
摘要 A gas turbine article includes a substrate, a plurality of geometric surface features that protrude from the substrate, and a thermally insulating topcoat disposed over the plurality of geometric surface features. The thermally insulating topcoat includes segmented portions that are separated by faults that extend through the topcoat from the geometric surface features.
申请公布号 US2011116920(A1) 申请公布日期 2011.05.19
申请号 US20090621557 申请日期 2009.11.19
申请人 STROCK CHRISTOPHER W;BUCHINA GENE;THOLEN SUSAN M 发明人 STROCK CHRISTOPHER W.;BUCHINA GENE;THOLEN SUSAN M.
分类号 F01D25/16;B32B3/30;B32B15/04;C23C4/10 主分类号 F01D25/16
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