Anti-icing system for aircraft

Details Anti-icing system for aircraft Anti-icing system for aircraft

1988-04-27

1990-12-11

Barefoot, Galen

Aeronautics and astronautics

Aircraft structure

Ice prevention

B64D 1504

Patent

active

049763970

ABSTRACT:
A deicing system for leading edges of an aircraft. There is a hot air supply tube extending along the leading edge, a fan to move air through the tube, compressor to heat the air that is moved through the tube, and pressure release valves. The hot air is discharged from openings in the tube to spray against the internal surfaces of the wall forming the leading edge.

REFERENCES:
patent: 1750777 (1930-03-01), Ingram
patent: 1864438 (1932-06-01), Janson
patent: 2766740 (1956-08-01), Brass
patent: 3917193 (1975-11-01), Runnels, Jr.

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