New-generation servo drive - thrust control actuator ПРТ-2-10 (control cassette and gear)
|■||Thrust control actuator ПРТ-2-10 is intended to automatically convert low-power control signals, which are issued by computers in the analogue form, into angular displacement of aircraft engines control levers at a rate proportional to the control signal voltage, and to provide thrust control switchover from automatic to manual mode.
|■||The actuator is a component part of aircraft piloting and navigation equipment.
|■||Nominal DC supply voltage
||27 V, 33 V
|■||Control signal dead band, max.
|■||Load torque on the output shaft
|■||Maximum turning angle of each output shaft
|■||Number of output shafts
|■||Rotation speed of electric actuators’ output shafts, min.
|■||Ambient temperature (operating)
||-55°С to +55°С