Air scoop lip warmer de-icing system

Aeronautics and astronautics – Aircraft power plants

Patent

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Details

60 39093, 244134R, 244134B, B64D 3302, B64D 1502, F02C 7045

Patent

active

044064314

ABSTRACT:
An elongated air scoop integrated with the engine housing for a jet prop powered aircraft is provided with a thin tubular metal manifold loop fitted to the open forward end of the air scoop and the hot exhaust gas bled from the engine exhaust system is continuously fed through the tubular loop which forms a hot defrost lip for the air scoop.

REFERENCES:
patent: 2655308 (1953-10-01), Luttman
patent: 3938761 (1976-02-01), Hempenstall
patent: 3981466 (1976-09-01), Shah
patent: 4240250 (1980-12-01), Harris
Jane's All The World's Aircraft, 1977-1978, Edition, Cessna 337 and 337 P Skymaster.

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