FIELD: aviation; measurement of intensity of icing and thickness of ice on flying vehicle.
SUBSTANCE: device includes first and second thermostabilizers, power difference separation unit, non-linear member, integrator and second indicator; first thermostabilizer is connected by its input to temperature sensor of working sensitive element and its output is connected to heater of working sensitive element; input of second thermostabilizer is connected to temperature sensor of compensating sensitive element and its output is connected to heat of compensating sensitive element.
EFFECT: enhanced accuracy of measurements and enhanced reliability.
1 dwg
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