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.	±0.25 V
■	Load torque on the output shaft	10.78 N•m
■	Maximum turning angle of each output shaft	96°
■	Number of output shafts	2
■	Rotation speed of electric actuators’ output shafts, min.	2.5 rpm
■	Ambient temperature (operating)	-55°С to +55°С
■	Actuator weight	5.5 kg