A lever control system integrates taxi operation using an electric motor in an aircraft with speed control of a jet engine in the same aircraft. The lever control system provides a smooth transition between the electric motor system used for aircraft taxi operation, and a jet engine system used to fly the aircraft. The lever control system may include a reverse lockout mechanism to prevent unintended reverse taxi movement of the aircraft.


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    Titel :

    Control panel integration into aircraft throttle control


    Weitere Titelangaben:

    Bedienfeldintegration in Flugzeugdrosselsteuerung
    Intégration d'un panneau de commande dans une commande des gaz d'un avion


    Beteiligte:
    OTT JOSEPH (Autor:in) / HUGHES KEITH (Autor:in) / DE MERS ROBERT E (Autor:in) / OLOFINBOBA OLUKAYODE (Autor:in)

    Erscheinungsdatum :

    01.07.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02D CONTROLLING COMBUSTION ENGINES , Steuern oder Regeln von Brennkraftmaschinen



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