A device for controlling a propeller, having variable-pitch blades, of a turboprop engine, has a first hydromechanical device for controlling the pitch of the blades of the propeller and a second hydromechanical device for controlling the speed of rotation of the propeller. The device includes a single electromechanical actuator with a movable actuator member mechanically connected both to the first hydromechanical device for controlling the pitch, in order to manage the pitch setpoint, and to the second hydromechanical device for controlling the speed, in order to manage the speed setpoint.
DISPOSITIF DE REGULATION D'UNE HELICE A PALES A CALAGE VARIABLE D'UN TURBOPROPULSEUR
2017-07-07
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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