| 摘要 |
The invention relates to a rotor (10) for a power plant, in particular an aero engine or a gas turbine, whereby said rotor (10) comprises at least two bonded rotor discs (12, 14). The rotor (10) is characterised in that an inlet opening (30) for inlet of fluid from around the rotor (10) into a chamber (26, 44) in one or between two adjacent rotor discs (12, 14) is provided and at least one interrupter element (38) with at least one fluid passage (40) is arranged in the chamber (26). |
