Deicer control system

Aeronautics and astronautics – Aircraft structure – Ice prevention

Patent

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Details

244134A, B64D 1500

Patent

active

047338342

ABSTRACT:
A deicer control circuit wherein a pressurized air source is connected to control valves and a regulating valve. Such regulating valve has a vacuum line output line that is also connected to such control valves. The control valves, on actuation by a timer, will sequence the pressure line and the vacuum line to alternately inflate and deflate the deicer units. The control valves also provide a sealing off or locking in of the pressurized deicer units in this sequence in response to a pressure sensor.

REFERENCES:
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patent: 2515519 (1950-07-01), Lawrence et al.
patent: 2912190 (1959-11-01), MacDonough
patent: 2934288 (1960-04-01), MacIntyre
patent: 3263702 (1966-08-01), Pallen et al.
patent: 3693916 (1972-09-01), Tritt et al.
patent: 3704720 (1972-12-01), Kaiser
patent: 3720388 (1973-03-01), Kaatz et al.

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