A control system for a component of a rescue hoist attached to an aircraft is disclosed. In various embodiments, the control system includes a first bus extending between a control module of the rescue hoist and a control input device; a second bus extending between the control module of the rescue hoist and the control input device; and a hardwire extending between the control module of the rescue hoist and the control input device.


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    Titel :

    Dual bus and hardwire architecture for high reliability control of helicopter hoist


    Beteiligte:
    BRYSON RICHARD (Autor:in) / RIEHLE OWEN (Autor:in) / LEINGANG ALAN F (Autor:in)

    Erscheinungsdatum :

    03.01.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B66C Krane , CRANES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B66D Haspeln , CAPSTANS / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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