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
2024-10-09
Patent
Electronic Resource
French
Dispositif d’aide à la régulation des hélices de turbomachines aéronautiques
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