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.
УСТРОЙСТВО РЕГУЛИРОВАНИЯ ВОЗДУШНОГО ВИНТА С ПЕРЕМЕННЫМ УГЛОМ УСТАНОВКИ ЛОПАСТЕЙ ТУРБОВИНТОВОГО ДВИГАТЕЛЯ
2019-07-24
Patent
Elektronische Ressource
Russisch
IPC: | B64C AEROPLANES , Flugzeuge |
УСТРОЙСТВО ДЛЯ РЕГУЛИРОВАНИЯ ОХЛАЖДАЮЩЕГО ВОЗДУШНОГО ПОТОКА В АВТОМОБИЛЕ
Europäisches Patentamt | 2017
СПОСОБ И УСТРОЙСТВО ДИСТАНЦИОННОГО ОСМОТРА СОСТОЯНИЯ ДВИГАТЕЛЯ ВОЗДУШНОГО СУДНА
Europäisches Patentamt | 2019