A torsional moment acting on a component in a drive train of an aircraft may be determined using at least one sensor, where the determined torsional moment is used for adjusting at least one adjustable damping element located in or on the component and/or for regulating a torsional stiffness in the torque-conducting component. As a result, the torsional load in the component may be reduced.
METHOD FOR DAMPING TORSIONAL VIBRATIONS IN A DRIVE TRAIN, AND DRIVE TRAIN
2021-09-09
Patent
Electronic Resource
English
Method for damping torsional vibrations in a drive train, and drive train
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