| 摘要 |
An apparatus and method for adjusting a bearing array, specifically for a gas turbine aircraft engine, is disclosed. The bearing array has a first stator-side, or fixed, bearing ring and a second rotor-side, or rotating, bearing ring, where rolling elements are located between the stator-side bearing ring and the rotor-side bearing ring. Transducers are assigned to the stator-side bearing ring to determine the position of the stator-side bearing ring and actuators govern the position of the stator-side bearing ring.
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