A method of providing power information in a rotorcraft, the rotorcraft having a powerplant. The method comprising calculating a real-time power required and calculating a real-time power available, and orienting power required and power available indicators on a power safety instrument, the position of the power required indicator being dependent upon the calculated power required, and the position of the power available indicator being dependent upon the calculated power available.


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    Title :

    POWER SAFETY INSTRUMENT SYSTEM


    Additional title:

    STROMSICHERHEITSSYSTEM
    SYSTÈME D'INSTRUMENTS DE SÉCURITÉ DE PUISSANCE


    Contributors:

    Publication date :

    2017-10-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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