发明名称 ABRADABLE COATINGS
摘要 PROBLEM TO BE SOLVED: To provide turbine shroud abradable coatings that balance contradictory requirements of high flowpath solidity, low blade tip wear, and high durability in service.SOLUTION: Shrouds 10 include a shroud substrate 12, a coating system, and an abradable coating 14. The coating system overlies at least a portion of an outer surface of the shroud substrate. The coating system includes a bond coat, a thermal barrier coating (TBC), and/or an environmental barrier coating (EBC). The abradable coating overlies at least a portion of the barrier coating. The abradable coating defines a substantially smooth continuous flowpath surface. The abradable coating includes a hybrid microstructure including a relatively dense, high-durability phase corralling relatively porous abradable phases. Second regions are more abradable by turbine blades 100 than first regions.
申请公布号 JP2016006320(A) 申请公布日期 2016.01.14
申请号 JP20150114387 申请日期 2015.06.05
申请人 GENERAL ELECTRIC CO <GE> 发明人 LIPKIN DON MARK;LUC STEPHANE LEBLANC
分类号 F01D11/12;C04B41/89;F01D5/08;F01D5/26;F01D5/28;F01D25/00;F02C7/00;F02C7/28 主分类号 F01D11/12
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