发明名称 Rotor blade for a gas turbine engine
摘要 The blade has a hollow tip portion with an internal surface 28 extending across the direction of the centrifugal field on the blade. A weight 29 comprising e.g. Silicon Nitride or Carbide is caused by centrifugal force to bear on the surface 28 such that relative motion and hence friction between the weight and the surface serves to damp vibration of the blade. <IMAGE>
申请公布号 GB2067675(A) 申请公布日期 1981.07.30
申请号 GB19800039142 申请日期 1980.12.10
申请人 ROLLS ROYCE LTD 发明人
分类号 F01D5/16;F01D5/18;(IPC1-7):F01D5/16 主分类号 F01D5/16
代理机构 代理人
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