A leg mechanism includes an articulated leg system (100), a passive device (130) and a cable (134). The articulated leg system (100) has a leg portion (128). The passive device (130) is coupled to the articulated leg system and is configured to apply a first force to a portion thereof. The cable (134) is coupled to the articulated leg system (100) and is configured to apply a second force, in opposition to the first force, to a portion thereof. When the cable (134) is drawn away from the articulated leg system (100), the second force moves the leg portion (128) in a first direction. When tension is released from the cable (134), the passive device (130) exerts the first force so as to move the leg portion (128) a second direction that is opposite the first direction.


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    Titel :

    Cable-Driven Four-Bar Link Leg Mechanism


    Beteiligte:
    DI LEO CLAUDIO V (Autor:in) / COSTELLO MARK F (Autor:in) / LEON BENJAMIN (Autor:in) / RIMOLI JULIAN JOSE (Autor:in) / WARD MICHAEL B (Autor:in)

    Erscheinungsdatum :

    24.09.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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