FIELD: automotive industry.
SUBSTANCE: in the method of heating the windshield of an aircraft three temperature sensors and the gear position sensor are mounted on the windshield, the readings of the gear position sensor and any two of the three sensors on the windshield are transmitted to the computer, the difference between which does not exceed 3°C. If the condition is not satisfied, then another pair of sensors from the three sensors on the windshield is selected. In the computer based on the information obtained the average value of readings of the selected pair of sensors from the windshield is determined, control information is formed and transmitted to the switch to switch on or switch off heating of the windscreen. At that at extended gear the windshield temperature is maintained in the range of 6-15°C, and in flight - in the range of 28-38°C.
EFFECT: accurate maintaining the temperature of the windshield with its uneven blowing, minimum load of the computer.
8 cl, 1 dwg
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Authors
Dates
2015-07-27—Published
2014-06-25—Filed