发明名称 ABRADABLE COATINGS
摘要 Turbine shroud abradable coatings that balance the apparently contradictory requirements of high flowpath solidity, low blade tip wear, and good durability in service. The shrouds include a shroud substrate (12), a coating system (20), 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. The second phases are relatively more abradable by the blades of a turbine than the second regions.
申请公布号 EP2955333(A1) 申请公布日期 2015.12.16
申请号 EP20150171046 申请日期 2015.06.08
申请人 GENERAL ELECTRIC COMPANY 发明人 LIPKIN, DON MARK;LEBLANC, LUC STEPHANE
分类号 F01D11/12 主分类号 F01D11/12
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