An actuator unit includes first and second link mechanisms. The first link mechanism has first and second arms that extend in first and second directions when viewed in a direction parallel to an axis of rotation. The first arm is connected at a first connection point to a power source for powering the first link mechanism. The second arm is connected at a second connection point to the second link mechanism. The second link mechanism is connected at a third connection point to a locking collar. The locking collar is configured to reciprocate as the first link mechanism rotates in a reciprocating manner. The distance from the first connection point to the axis of rotation is greater than the distance from the second connection point to the axis of rotation.


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    Titel :

    ACTUATOR UNIT


    Beteiligte:
    ITO KOJI (Autor:in)

    Erscheinungsdatum :

    15.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein / B64C AEROPLANES , Flugzeuge



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