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.


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    Titel :

    METHOD FOR DAMPING TORSIONAL VIBRATIONS IN A DRIVE TRAIN, AND DRIVE TRAIN


    Beteiligte:
    WOLF DANIEL (Autor:in) / LITZBA JÖRG (Autor:in) / SCHÄFER JOHANNES (Autor:in) / TENCKHOFF GEORG (Autor:in)

    Erscheinungsdatum :

    09.09.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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