This control device for a propulsion system, comprising means for calculating a blade-pitch setpoint of at least one propeller of the propulsion system, the calculation means using a performance predictive model of the propeller taking account of at least one flight speed for adapting a blade-pitch angle setpoint, is characterised in that the performance predictive model of the propeller is configured to use polar charts implemented in the form of a mathematical law.
DISPOSITIF D'AIDE À LA RÉGULATION DES HÉLICES DE TURBOMACHINES AÉRONAUTIQUES
DEVICE FOR ASSISTING WITH REGULATION OF PROPELLERS OF AERONAUTICAL TURBOMACHINERY
HILFSVORRICHTUNG ZUR REGULIERUNG VON PROPELLERN EINER AERONAUTISCHEN TURBOMASCHINE
09.10.2024
Patent
Elektronische Ressource
Französisch
Dispositif d’aide à la régulation des hélices de turbomachines aéronautiques
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