A feedback system controlled by a computer monitors the variation in power transmitted through the servo mechanism (13, fig 2),15,(20),22 for a flying control surface during an aerobatic manoeuvre initiated by the control surface, and applies to the flying control lever 12 a feedback force which is representative of the variation in power. The tactile force is relatively weak when the aerobatic manoeuvre is performed at a speed close to stalling speed and is relatively strong when the aerobatic manoeuvre is performed at a speed close to the maximum permissible speed at cruising altitudes.


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    Titel :

    Improvements in aircraft


    Beteiligte:

    Erscheinungsdatum :

    08.07.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64C AEROPLANES , Flugzeuge



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