A method of assisting the piloting of an aircraft, such as a helicopter, includes determining a limiting power margin of a power plant of the aircraft relative to a power limit at an operating rating of an engine of the power plant. The limiting power margin is transformed into a collective pitch margin for the operating rating. The collective pitch margin represents the margin between a current collective pitch of blades of a main rotor of the aircraft and a collective pitch limit of the blades of the main rotor. The collective pitch limit is determined and then displayed on a display of the aircraft for a pilot to view.


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    Title :

    PROCÉDÉ, DISPOSITIF D'AIDE AU PILOTAGE D'UN AÉRONEF, ET AÉRONEF


    Additional title:

    A METHOD AND A DEVICE FOR ASSISTING THE PILOTING OF AN AIRCRAFT, AND AN AIRCRAFT
    VERFAHREN UND HILFSVORRICHTUNG ZUR STEUERUNG EINES LUFTFAHRZEUGS, UND LUFTFAHRZEUG


    Contributors:

    Publication date :

    2018-09-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

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



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