| 摘要 |
A gas turbine machine comprises at least one blade cluster (10), in which several blades (12) are arranged on a common inner ring (14) and/or outer ring (16). The blade cluster (10) has at least one hollow space (18), inside which several damping elements (20, 22, 24) are provided that can be independently moved relative to the walls of the hollow space (18) and relative to one another. |
