| 摘要 |
A rotor (10) for a power plant, in particular an aero engine or a gas turbine, whereby the rotor (10) includes at least two bonded rotor discs (12, 14). The rotor (10) has 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) and at least one interrupter element (38) with at least one fluid passage (40) is arranged in the chamber (26).
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