发明名称 LOW PERMEABILITY HIGH PRESSURE COMPRESSOR ABRADABLE SEAL FOR BARE NI AIRFOILS HAVING CONTINUOUS METAL MATRIX
摘要 An air seal (60) in a gas turbine engine (10) comprising a substrate (40). A bond coating layer (65) is adhered to the substrate (40). An abradable layer (70) is adhered to the bond coating layer (65). The abradable layer (70) comprises a metal matrix discontinuously filled with a soft ceramic material.
申请公布号 EP2937437(A1) 申请公布日期 2015.10.28
申请号 EP20150164502 申请日期 2015.04.21
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 STROCK, CHRISTOPHER W.
分类号 C23C4/00;F01D11/12 主分类号 C23C4/00
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