| 摘要 |
A balancing device, particularly for turbocompressors, comprising a base structure which supports elastically a supporting structure which has a flange for supporting a receptacle of a rotating element and a rotating element, wherein the rotating element can move with a rotary motion about its own rotation axis; actuation elements being adapted to actuate lever elements along a substantially radial direction; the lever elements being adapted to generate a force for fixing the receptacle of the rotating element to the supporting flange in a direction that is substantially parallel to the rotation axis.
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