USAGE BASED PROPELLER LIFE MONITORING

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...

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Bibliographische Detailangaben
Hauptverfasser:	VIGNALI, Mark, HUTH, Brian P, LACROIX, Olivier, EL HALOUI, Abdellah
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS MEASURING PARACHUTES PERFORMING OPERATIONS PHYSICS TESTING TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR TRANSPORTING
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Beschreibung
Zusammenfassung:	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