| 摘要 |
A damper system (90) for a turbine having adjacent turbine bucket platforms (104) including opposing slash faces (122) having opposing grooves (126) is provided. The system includes a pin having a substantially cylindrical-shaped body (129) configured for positioning in the opposing grooves (126). A set of slots (130, 230) are provided in an outer surface (132) of the pin and at spaced axial locations therealong. The set of slots (130, 230) face in a radially outward direction relative to the turbine bucket platforms (104). |
