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.


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    Title :

    УСТРОЙСТВО РЕГУЛИРОВАНИЯ ВОЗДУШНОГО ВИНТА С ПЕРЕМЕННЫМ УГЛОМ УСТАНОВКИ ЛОПАСТЕЙ ТУРБОВИНТОВОГО ДВИГАТЕЛЯ


    Publication date :

    2019-07-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge