FIELD: flying vehicle equipment.
SUBSTANCE: proposed system includes thermal gas jet pump, pressure sensor, switchgear with automatic flow-type gas sample analyzer made in form of electrochemical sensor mounted in thermostat and gas medium condensate trap. Gas sample analyzer is made in form of electrochemical primary transducer mounted in thermostat and second transducer which are electrically interconnected. Primary transducer includes electrochemical cell, temperature sensor and heater for preheating the electrolyte. Secondary transducer includes amplifier, pressure and temperature compensating units, time correction unit and heater control unit.
EFFECT: enhanced reliability of monitoring.
3 dwg
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