A vibrotactile system for an aircraft may comprise a plurality of tactors and a tactor driver operably coupled to the plurality of tactors. The tactor driver may be configured to determine a vibration sequence for the plurality of tactors in response to a signal received from an aircraft controller, and to send vibration commands corresponding to the vibration sequence to the plurality of tactors.


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    Titel :

    VIBROTACTILE SYSTEMS AND METHODS FOR AIRCRAFT SEATS


    Beteiligte:
    HAMPTON JOHN L (Autor:in) / SHAW GLEN (Autor:in) / FAHEY TYLER (Autor:in) / BORCHELT DONALD (Autor:in) / SKOLA JOHN R (Autor:in) / MISHKIN ROBERT (Autor:in)

    Erscheinungsdatum :

    14.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B60N SEATS SPECIALLY ADAPTED FOR VEHICLES , Sitze besonders für Fahrzeuge ausgebildet / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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