FIELD: aviation.
SUBSTANCE: device for air removal from the working fluid of the closed hydraulic systems of aircrafts comprises hydraulic pump with independent drive and hydraulic tank. Hydraulic pump is connected to the pressure line, suction line and fittings for connection to the onboard valves of pump and suction mains of the serviced hydraulic system. Hydraulic tank consists of confuser and tube, one end of which is connected to the pipeline of suction line, and the second is designed in the form of nozzle and touches the confuser wall. Confuser is rigidly attached to the body of hydraulic tank via the disk with apertures.
EFFECT: improving the working conditions of hydraulic system of the aircraft.
2 dwg
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