Icing hazard detection for aircraft

Communications: directive radio wave systems and devices (e.g. – Radar for meteorological use

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342 22, 342460, G01S 1338, G01S 1395

Patent

active

050289292

ABSTRACT:
An airborne Icing Hazard Detector for aircraft uses dual frequency radar beams which are transmitted into a cloud ahead of the aircraft. The reflected signals at each of the two frequencies are compared and processed to determine the presence, amount and location of regions of liquid water in the cloud. The presence of liquid water is determined as a result of liquid water attenuating the power of one of the signals a greater amount than the other signal, due to different attenuation characteristics of the two signals at the two frequencies. A temperature sensor provides ambient temperature information to determine if the detected liquid water is super-cooled. Upon detection of a predetermined amount of liquid water and the determination that it is super-cooled, an advance warning indication is provided to allow the pilot to avoid flying through the volumetric region of supercooled liquid water and risking ice formation on the aircraft.

REFERENCES:
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patent: 4015257 (1977-03-01), Fetter
patent: 4050067 (1977-09-01), Elmore, Jr.
patent: 4075555 (1978-02-01), Wight et al.
patent: 4613938 (1986-09-01), Hansen et al.
D. Atlas, "The Estimation of Cloud Parameters by Radar", II, Journal of Meteorology, pp. 309-317 (Aug. 1954).
J. Goldhirsh and I. Katz, "Estimation of Raindrop Size Distribution Using Multiple Wavelength Radar Systems", ti Radio Science, vol. 9, No. 4, pp. 439-446 (Apr. 1974).
W. Sand et al, "Icing Conditions Encountered by a Research Aircraft", 23, Journal of Climate and Applied Meteorology, pp. 1427-1440 (Oct. 1984).
M. Politovich, "Measurements of Hazardous Icing Conditions", 3rd Int'l. Conference on the Aviation Weather System, Anaheim, Calif., 29 Jan.-3 Feb., 1989.

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