Microwave deicing for aircraft engine propulsor blades

Electric heating – Metal heating – Of cylinders

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219 1055F, 219 1055R, 244134D, 340581, H05B 680, B64D 1512

Patent

active

050618369

ABSTRACT:
A deicing system for an aircraft engine (4) having blades (14, 16) fixedly attached to rotating propulsors (6, 8) has emitters (22, 28) which irradiate microwave beams (24, 26, 30 32) onto coatings (18, 20) which are fixedly attached to said blades (14, 16). Substantially more of the energy of the beams (24, 26, 30, 32) is absorbed by the coatings (18, 20) than by any water or ice on the blades (14, 16) causing any ice which is on the blades (14, 16) to be thrown off by the centrifugal force of the rotating propulsors (6, 8).

REFERENCES:
patent: 3397302 (1968-08-01), Hosford
patent: 4054255 (1977-10-01), Magenheim
patent: 4060212 (1977-11-01), Magenheim
patent: 4267420 (1981-05-01), Brastad
patent: 4365131 (1982-12-01), Hansman, Jr.
patent: 4876178 (1989-10-01), Voss et al.

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