发明名称 Turbine engine rotor retainer
摘要 A gas turbine engine has a rotor stack carried by a central shaft. A number of retainer segments each have a first surface engaging the rotor stack and a second surface engaging the central shaft so as to transmit a precompression force from the central shaft to the rotor stack.
申请公布号 US2005232774(A1) 申请公布日期 2005.10.20
申请号 US20040825256 申请日期 2004.04.15
申请人 SUCIU GABRIEL L;NORRIS JAMES W 发明人 SUCIU GABRIEL L.;NORRIS JAMES W.
分类号 F02C7/00;F01D5/02;F01D5/06;F01D11/00;(IPC1-7):H02K5/16 主分类号 F02C7/00
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