FIELD: machine building.
SUBSTANCE: proposed power amplifier is designed for aircraft electrohydraulic automatic control systems. The amplifier comprises the 1st adding operating amplifier with its one input receiving the control signal and the other one being connected, via matching hardware, with the feed back transducer signal winding. It includes also the electronic power amplifier with its output connected to the electro mechanic converter, 1st stage hydraulic control valve communicating with intake and discharge lines and, via two hydraulic lines, with the 2nd stage hydraulic valve control chambers. The 1st correcting device is arranged at the 1st adding operating amplifier. The output of the former is connected to one of the inputs of the 2nd adding operating amplifier. The 2nd output of the latter is connected to the output of the 3rd electronic correcting device with its input being connected to the output of matching hardware. The output of the 2nd electronic correcting device is connected to the electronic power amplifier input.
EFFECT: improved static, dynamic and power performances of hydraulic amplifier.
1 dwg
Authors
Dates
2009-07-10—Published
2007-07-10—Filed