An aircraft with a control system having joint control for a throttle and a propeller of an aircraft may be modified to decouple the joint control of a throttle and a propeller. Control of the throttle and propeller may be independent of the other. Exemplary modification of a control system may use new structures, existing structures, repurpose existing structures, or use a combination thereof. Additionally or alternatively, modification of a control system may provide controls with tactile distinction to a user.


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    Titel :

    Control quadrant


    Beteiligte:
    GUIDA NICHOLAS R (Autor:in) / KOEHLER DIETER (Autor:in) / GATES HALDAN R (Autor:in) / BABIN STEPHEN L (Autor:in) / MITCHELL DWIGHT W (Autor:in) / HRDINA CHASE (Autor:in)

    Erscheinungsdatum :

    06.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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