Device for preventing ice formation on parts of aircraft

Aeronautics and astronautics – Aircraft structure – Ice prevention

Patent

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B64D 1512

Patent

active

040210081

ABSTRACT:
A device for preventing ice formation on parts of aircraft-support surfaces (wings or aerofoils), propellers, rotor blades or the like-comprises electrical resistance heaters embedded in a shell of thermally conducting material (e.g. aluminium sheet or moulding) sheathing the aircraft part. Thermally insulating, thermally conducting and electrically insulating layers may be provided within the shell. The heaters, or some of them, may be controlled by a temperature sensor in or on the shell.

REFERENCES:
patent: 1021230 (1912-03-01), Ball
patent: 2297540 (1942-09-01), Driscoll
patent: 2552075 (1951-05-01), Van Daam
patent: 2649267 (1953-08-01), Luke
patent: 2762897 (1956-09-01), Vrooman et al.
patent: 2802087 (1957-08-01), Chilman
patent: 3409759 (1968-11-01), Boicey et al.
patent: 3465121 (1969-09-01), Clark

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