A vibrotactile system for an aircraft may comprise a plurality of tactors (122, 124) and a tactor driver (130) operably coupled to the plurality of tactors (122, 124). The tactor driver (130) may be configured to determine a vibration sequence for the plurality of tactors (122, 124) 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 (122, 124).


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    Title :

    VIBROTACTILE SYSTEMS AND METHODS FOR AIRCRAFT SEATS


    Additional title:

    VIBROTAKTILE SYSTEME UND VERFAHREN FÜR FLUGZEUGSITZE
    SYSTÈMES VIBROTACTILES ET PROCÉDÉS POUR SIÈGES D'AVION


    Contributors:
    HAMPTON JOHN L (author) / SHAW GLEN (author) / FAHEY TYLER (author) / BORCHELT DONALD (author) / SKOLA JOHN R (author) / MISHKIN ROBERT (author)

    Publication date :

    2023-12-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G08B SIGNALLING OR CALLING SYSTEMS , Signalisier- oder Rufsysteme / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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