发明名称 INTERLOCKING HOLE PATTERN SEAL
摘要 A seal for a turbomachine is disclosed. The seal assembly includes a rotatable shaft having a stepped outer circumferential surface that defines one or more annular protrusions axially-spaced thereon. A seal is radially-offset from the rotatable shaft and has one or more annular recesses that extend radially-outward from the inner circumferential surface of the seal. A plurality of holes are defined in both the inner circumferential surface and the one or more annular recesses of the seal, the one or more annular recesses being axially-spaced from each other and configured to receive the one or more annular protrusions in an interlocking fit.
申请公布号 WO2012129475(A2) 申请公布日期 2012.09.27
申请号 WO2012US30279 申请日期 2012.03.23
申请人 DRESSER-RAND COMPANY;GUPTA, MANOJ K.;NOVE, STEVEN;SOULAS, THOMAS;RAMESH, KRISHNASWAMY;GROSSO, GLENN 发明人 GUPTA, MANOJ K.;NOVE, STEVEN;SOULAS, THOMAS;RAMESH, KRISHNASWAMY;GROSSO, GLENN
分类号 F16J15/24;F16J15/16 主分类号 F16J15/24
代理机构 代理人
主权项
地址