The present invention relates to a drive system for an aircraft More specifically, it relates to a fully electric speed-proportional control and drive system for the nose wheel of an aircraft wherein variable steering authority is accomplished by monitoring of the signal from a tiller and rudder pedals by a nose wheel controller in conjunction with the speed of the aircraft, in order to command and power an electromechanical steering, actuator to achieve speed-proportional variable steering authority. This provides a system with a quicker response time than current hydraulic-based systems which can help reduce nose wheel shimmy, elimination of certain nose wheel steering failure modes associated with hydraulic systems and has a reduced weight when used in small-to-medium sized aircraft.


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    Titel :

    FULLY ELECTRIC SPEED-PROPORTIONAL NOSE WHEEL STEERING SYSTEM FOR AN AIRCRAFT


    Weitere Titelangaben:

    SYSTEME DE DIRECTION DE ROUE AVANT PROPORTIONNELLE A LA VITESSE ENTIEREMENT ELECTRIQUE DESTINE A UN AERONEF


    Beteiligte:
    SHARPE PETER (Autor:in)

    Erscheinungsdatum :

    07.06.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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