A vibration reduction apparatus according to the present invention includes: an actuator apply a force to a beam supporting a cabin so as to bend the beam; an acceleration sensor measuring the acceleration of the cabin; and a controller controlling the actuator based on the measured acceleration. When a vibration containing a plurality of vibration components is transmitted to the cabin via the beam, the vibration reduction apparatus thus structured can achieve the vibration reduction more certainly by applying a bending load to the beam so that the bending load caused by the vibration is cancelled; this allows providing damping of the cabin more certainly.


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    Titel :

    HELICOPTER AND VIBRATION REDUCTION METHOD


    Weitere Titelangaben:

    HUBSCHRAUBER UND SCHWINGUNGSDÄMPFUNGSVERFAHREN
    HÉLICOPTÈRE ET PROCÉDÉ DE RÉDUCTION DES VIBRATIONS


    Beteiligte:
    YOSHIZAKI YUJI (Autor:in) / ITO HIROSHI (Autor:in) / SUZUKI HIDETOSHI (Autor:in)

    Erscheinungsdatum :

    2020-05-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge / H01L Halbleiterbauelemente , SEMICONDUCTOR DEVICES




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