To provide vibrotactile systems for aircraft seats, and methods for operating the vibrotactile systems for aircraft seats.SOLUTION: 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.SELECTED DRAWING: Figure 3

    【課題】 航空機シートの振動触覚システム、及び航空機シートの振動触覚システムの動作方法を提供する。【解決手段】 航空機の振動触覚システムは、複数の触覚器と、複数の触覚器に動作可能に接続された触覚器ドライバとを備え得る。触覚器ドライバは、航空機コントローラから受信した信号に応答して、複数の触覚器の振動シーケンスを決定し、振動シーケンスに対応する振動コマンドを、複数の触覚器に送信するように構成され得る。【選択図】図3


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    Title :

    VIBROTACTILE SYSTEMS FOR AIRCRAFT, METHODS FOR OPERATING THE SAME, AND EJECTION SEATS


    Additional title:

    航空機の振動触覚システム、その動作方法、および射出シート


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

    Publication date :

    2023-12-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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