Detector for indicating ice formation on the wing of an aircraft

Aeronautics and astronautics – Aircraft structure – Ice prevention

Patent

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Details

340582, 73599, B64D 1522

Patent

active

054679443

ABSTRACT:
A detector indicating ice formation on the wing of an aircraft or any planear surface, based on a thread-like or a tape-like transducer, through which an ultrasonic signal is transmitted at one end. The attenuation of the signal having passed through the thread is measured with a receiver at the opposite end while the thread is simultaneously being heated such that ice that may surround it melts again, the attenuation thus resuming its initial level.

REFERENCES:
patent: 2419454 (1947-04-01), Le Clair
patent: 3412326 (1968-11-01), Jones et al.
patent: 3541540 (1970-11-01), Hughes
patent: 4054255 (1977-10-01), Magenheim
patent: 4335613 (1982-06-01), Luukkala
patent: 4461178 (1984-07-01), Chamuel
patent: 4604612 (1986-08-01), Watkins et al.

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