Aeronautics and astronautics – Aircraft structure – Ice prevention
Patent
1985-03-08
1987-01-27
Basinger, Sherman D.
Aeronautics and astronautics
Aircraft structure
Ice prevention
244134F, 219497, B64D 1512
Patent
active
046389601
ABSTRACT:
A method of determining the temperature, preferably the ice boundary temperature, of an electrical resistive heating element of a de-icing system for airplanes, helicopters, and the like, preferably for a fully automatic control of the heating times of the heating elements. Additional temperature sensors are avoided and circuitry costs are substantially reduced by using the resistive heating elements themselves for determining the temperature. The resistance variation due to temperature variations of an element is ascertained by a current-voltage measurement, and a temperature variation of the element is determined from the resistance variation while using the temperature coefficient. The current-voltage measurement may be based on Ohm's law with a following analog or digital processing of the signal.
REFERENCES:
patent: 2767294 (1956-10-01), Fraser et al.
patent: 3277459 (1966-10-01), Werner
patent: 4514619 (1985-04-01), Kugelman
Loos Hans
Straube Axel
Basinger Sherman D.
Corl Rodney
Licentia Patent-Verwaltungs-GmbH
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