The invention relates to a method for monitoring at least one aircraft engine, said method including an acquisition (100) according to the first and second sets of measurements of respectively endogenous and exogenous variables. The method also includes:a normalization (200) of the measurements of the first set relative to the measurements of the second set,a generation (300) of a current model representative of the evolution of the behavior of the engine based on the normalized measurements,a detection (400) of potential abnormality in the behavior of the engine based on a comparison of the current model with a reference model,a generation (500) of a maintenance message,a transmission (600) of said ground message,the acquisition, normalization, generation of a current model, the detection and generation of a maintenance message being made on board the aircraft.
PROCEDE ET DISPOSITIF DE SURVEILLANCE D'AU MOINS UN MOTEUR D'AERONEF
METHOD AND DEVICE FOR MONITORING AT LEAST ONE AIRCRAFT ENGINE
VERFAHREN UND VORRICHTUNG ZUR ÜBERWACHUNG MINDESTENS EINES FLUGZEUGTRIEBWERKS
2023-05-03
Patent
Electronic Resource
French
IPC: | G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS |
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