FIELD: aviation.
SUBSTANCE: regional aircraft remote control system contains the main pitch, roll and yaw control levers, left and right ailerons, left and right sections of the elevator, rudder, hydraulic systems, electro-hydraulic steering actuators on the left and right sections of the elevator, rudder associated with hydraulic systems and with a block of calculators for control algorithms of electro-hydraulic steering gears, an alternating current electrical system. The left and right sections of the elevator and the rudder also contain servos and electromechanical steering gears associated with the servos connected to the AC electrical system. The system also contains a block of computers for control algorithms of electromechanical drives and a block for measuring the angular velocities of the aircraft.
EFFECT: increased flight safety, reduced weight of the control system and simplified maintenance.
1 cl, 1 dwg
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