The invention relates to a control device for an engine, comprising means (150) for calculating a blade pitch angle setpoint (160) of at least one propeller of the engine, the calculating means (150) using a propeller performance model, taking into account at least one flight speed (115) in order to adapt a blade pitch angle setpoint by taking into account a shaft horsepower setpoint.
Control device for an engine
2015-09-23
Patent
Electronic Resource
English