A method comprises operating a propeller (29) in-flight, receiving propeller vibration data during operation of the propeller (29) in-flight, computing, after at least one flight of an aircraft (100), an average vibration magnitude and an average vibration phase angle based on the propeller vibration data, determining a propeller balancing solution based on the average vibration magnitude and the average vibration phase angle, and generating a balancing need indication by outputting the propeller balancing solution.


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    Title :

    SYSTEM AND METHOD FOR PROPELLER BALANCING


    Additional title:

    SYSTEM UND VERFAHREN FÜR PROPELLERAUSGLEICH
    SYSTÈME ET PROCÉDÉ D'ÉQUILIBRAGE D'HÉLICE



    Publication date :

    2022-04-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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