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The present invention relates to a blade arrangement with damping elements and to a method of damping vibrations of a blade arrangement. The blade arrangement comprises a rotor and blades arranged on the circumference of the rotor. Damping elements (2, 3) are arranged between the blades and are in c

The present invention relates to a blade arrangement with damping elements and to a method of damping vibrations of a blade arrangement. The blade arrangement comprises a rotor and blades arranged on the circumference of the rotor. Damping elements (2, 3) are arranged between the blades and are in contact with the blades due to a centrifugal force, acting in the radial direction, during rotation of the rotor. In this case, at least two damping elements (2, 3) are arranged one behind the other in the circumferential direction of the rotor between adjacent blades, which damping elements (2, 3), during rotation of the rotor, come into contact with one another via a contact surface (6), and of which a first damping element (2) comes into contact with a first friction surface (4) of one of the blades and a second damping element (3) comes into contact with a second friction surface (5) of the other blade.A multiplicity of different vibration states can be effectively damped with the blade arrangement.

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1. A blade arrangement, comprising:a rotor; blades arranged at the circumference of the rotor; at least one set of damping elements arranged between at least two adjacent blades, said at least one set of damping elements comprising at least a first damping element and a second damping element arrang

1. A blade arrangement, comprising:a rotor; blades arranged at the circumference of the rotor; at least one set of damping elements arranged between at least two adjacent blades, said at least one set of damping elements comprising at least a first damping element and a second damping element arranged one behind the other in the circumferential direction of the rotor, wherein said first damping element and said second damping element of said at least one set of damping elements have different geometrical shapes, and the damping elements being arranged such that, during rotation of the rotor, due to a centrifugal force acting in the radial direction of the rotor, the damping elements arranged one behind the other in the circumferential direction of the rotor come into contact with one another at at least one contact surface, and the first damping element of said at least one set of damping elements comes into contact with a first friction surface of a first adjacent blade, and the second damping element of said at least one set of damping elements comes into contact with a second friction surface of a second adjacent blade.