发明名称 HIGH TEMPERATURE EROSION RESISTANT, ABRADABLE THERMAL BARRIER COMPOSITE COATING
摘要 A composite thermal barrier coating system includes a honeycomb metallic structure (2) filled with high thermal expansion ceramic hollow spheres (6) in a phosphate bonded matrix. The composite thermal barrier coating system may be manufactured to thicknesses (T) in excess of current thermal barrier coating systems, thereby imparting greater thermal protection. Superior erosion resistance and abrasion properties are also achieved. The composite thermal barrier coating is useful on combustion turbine components such as ring seal segments, vane segment shrouds, transitions and combustors.
申请公布号 WO0052307(A1) 申请公布日期 2000.09.08
申请号 WO2000US05105 申请日期 2000.02.28
申请人 SIEMENS WESTINGHOUSE POWER CORPORATION 发明人 MERRILL, GARY, B.;MORRISON, JAY, A.
分类号 C23C4/02;C23C26/02;C23C28/00;F01D5/28;F01D11/12;F23R3/00 主分类号 C23C4/02
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