发明名称 LOW PERMEABILITY HIGH PRESSURE COMPRESSOR ABRADABLE SEAL FOR BARE Ni AIRFOILS HAVING CONTINUOUS METAL MATRIX
摘要 An air seal in a gas turbine engine comprising a substrate. A bond coating layer is adhered to the substrate. An abradable layer is adhered to the bond coating layer. The abradable layer comprises a metal matrix discontinuously filled with a soft ceramic material.
申请公布号 US2015308281(A1) 申请公布日期 2015.10.29
申请号 US201514689492 申请日期 2015.04.17
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 STROCK CHRISTOPHER W.
分类号 F01D11/12;C23C4/10;C23C4/06 主分类号 F01D11/12
代理机构 代理人
主权项 1. A seal comprising: an abradable layer, the abradable layer comprising a metal matrix discontinuously filled with soft ceramic material clad with a metal.
地址 HARTFORD CT US