FIELD: engines and pumps.
SUBSTANCE: drive is intended for systems of aircraft control. Drive comprises double-cascade electric hydraulic power amplifier, the first summating operational amplifier, matching equipment, electric sensor of hydraulic cylinder feedback, the second summating operational amplifier, electronic power amplifier, electromechanical converter, at the outlet of the first summating operational amplifier the first electronic correction device is installed, outlet of the first electronic correction device is connected to input of electronic limitation unit, outlet of limitation unit is connected to one of inputs of summating operational amplifier, the second inlet of which is connected to outlet of the second electronic correction device, inlet of which is connected to outlet of matching equipment, outlet of the second summating operational amplifier is connected to inlet of electronic power amplifier.
EFFECT: simplification of electric hydraulic follower drive design.
1 dwg
