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
2022-04-20
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
SAE Technical Papers | 1945
|