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In a device for reducing resonant vibrations of rotor blades in turbomachines, cavities for the selective disturbance of the flow are arranged between the rotating blade tip and that wall of the casing which bounds the flow duct. These cavities are arranged in the casing wall in the region of the bl

In a device for reducing resonant vibrations of rotor blades in turbomachines, cavities for the selective disturbance of the flow are arranged between the rotating blade tip and that wall of the casing which bounds the flow duct. These cavities are arranged in the casing wall in the region of the blade tips and comprise a plurality of cavities arranged over the circumference. Their open cross section facing the flow duct is arranged in the axial planes bounded by the inlet edges and outlet edges of the rotor blades.

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A method for operating a device for reducing one or more resonant vibrations of rotor blades in turbomachines including at least one cavity provided in a casing wall in the region of rotor blade tips for disturbing a flow between a rotating blade tip and the casing wall which bounds a flow duct, sai

A method for operating a device for reducing one or more resonant vibrations of rotor blades in turbomachines including at least one cavity provided in a casing wall in the region of rotor blade tips for disturbing a flow between a rotating blade tip and the casing wall which bounds a flow duct, said cavities being arranged over a circumference of the casing, and arranged at least partially between axial planes bounded by an inlet edge and an outlet edge of the rotor blades at an open cross section of the circumference facing the flow duct, comprising the steps of: determining a rotary frequency causing the resonance; selecting a blade vibration to be suppressed, said vibration being associated with a k5h rotary frequency of the rotary; and, distributing the cavities for disturbing the flow over the circumference in such a way that an excitation with a kth multiple of the rotary frequency takes place, a sum of the angular positions of successive cavities in the circumferential direction being chosen so that the blade vibrations are reduced.