A system for monitoring propeller (102) health comprising:a processing unit having a processor (300) which is programmed to apply a plurality of algorithms to inputted aircraft parameter data (10);a plurality of data inputs for inputting aircraft parameter data (10) into the algorithms, wherein the processor (300) is configured to apply the physics based algorithms to the aircraft parameter data (10) to determine at least the fatigue life consumption (18) of one or more critical components of a propeller (102);and an output device 400, 500 which is able to output an indication of the determined fatigue life consumption (18) to an observer
USAGE BASED PROPELLER LIFE MONITORING
NUTZUNGSBASIERTE ÜBERWACHUNG DER PROPELLERLEBENSDAUER
SURVEILLANCE DE LA DURÉE DE VIE D'UNE HÉLICE BASÉE SUR L'UTILISATION
2021-09-01
Patent
Electronic Resource
English