| 摘要 |
Rotor (1) for turbomachines having a plurality of blades, and wherein a damping member (23; 123), housed inside a respective chamber (20) arranged between the two blades (5) of each pair of adjacent blades (5) of said rotor (1), is pushed, in use, by the centrifugal force against two surfaces (21), each of which is carried by a respective blade (5), which limit the respective chamber (20) in a radially outward direction; the damping member (23; 123) being cup-shaped and being provided with a base wall (24) facing the two surfaces of the relative chamber (20) and having three support bosses (25) on both of said surfaces (21). |
