Propeller deicer

Aeronautics and astronautics – Aircraft structure – Ice prevention

Patent

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Details

B64D 1512

Patent

active

043867499

ABSTRACT:
A deicer for use on the propeller of an aircraft wherein the heating elements or elements of the deicer which are embedded in an electrically non-conductive material adhered to a propeller blade provide a gradient type of heat distribution pattern having the greatest heat concentration at the area of the propeller closer to the shank end and a lower heat concentration at the area of the propeller further away from the shank end.

REFERENCES:
patent: 2494625 (1950-01-01), Martin
patent: 2552075 (1951-05-01), Van Daam
patent: 2599059 (1952-06-01), Jones
patent: 2757273 (1956-07-01), Taylor
patent: 3657514 (1972-04-01), Adams

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