发明名称 Turbine blade assembly with stranded wire cable dampers
摘要 A turbine blade assembly for a turbine assembly includes a turbine blade having a turbine blade damper cavity formed therein and stranded wire cable positioned within the turbine blade damper cavity. The stranded wire cable is maintained in the damper cavity during operation of the turbine blade assembly. It reduces vibration of the turbine blade assembly during operation by dissipating energy by friction between the stranded wire cable and the internal surface of the blade that defines the damper cavity. It also dissipates energy by friction between adjacent wires within the stranded wire cable.
申请公布号 US6685435(B2) 申请公布日期 2004.02.03
申请号 US20020133057 申请日期 2002.04.26
申请人 THE BOEING COMPANY 发明人 DAVIS GARY A.;TUTTLE GARY E.;BEATTY ROBERT F.
分类号 F01D5/16;F01D5/26;(IPC1-7):F01D5/26 主分类号 F01D5/16
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