发明名称 Turbine blade damper
摘要 A vibration damper for use in a turbine rotor of a high temperature gas turbine is disclosed. The damper is loosely mounted in an opening formed between adjacent blade rails, the end of the rotor disk connector, and sections of adjacent blade necks between the rails and the disk connector. A cover plate positioned against one side of the turbine blade and a projection extending downwardly from the other side of the turbine blade confines the damper axially in the opening.
申请公布号 US4182598(A) 申请公布日期 1980.01.08
申请号 US19770828457 申请日期 1977.08.29
申请人 UNITED TECHNOLOGIES CORP 发明人 NELSON, CHARLES J
分类号 F01D5/22;(IPC1-7):F01D5/10 主分类号 F01D5/22
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