发明名称 Spall resistant abradable turbine air seal
摘要 An abrasive coating (60) for a rotor shaft (50), the abrasive coating having a metal bond coat layer (62) on the rotor shaft and an abrasive layer (66) over the bond layer for contact with vanes (26) during operation of the rotor shaft. The abrasive coating includes a matrix containing a low strength filler having an increased concentration radially outward from the bond layer to the outer surface of the abrasive layer. The matrix may be ceramic or metal.
申请公布号 EP2540868(A1) 申请公布日期 2013.01.02
申请号 EP20120173070 申请日期 2012.06.21
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 STROCK, CHRISTOPHER W.;BAUMANN, PAUL W.
分类号 C23C28/00 主分类号 C23C28/00
代理机构 代理人
主权项
地址
您可能感兴趣的专利