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.
SYSTEM AND METHOD FOR PROPELLER BALANCING
SYSTEM UND VERFAHREN FÜR PROPELLERAUSGLEICH
SYSTÈME ET PROCÉDÉ D'ÉQUILIBRAGE D'HÉLICE
20.04.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |