Device for detecting and preventing the formation of ice on cont

Aeronautics and astronautics – Aircraft structure – Ice prevention

Patent

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Details

244134B, 244134F, B64D 1504, B64D 1518, B64D 1522

Patent

active

045082952

ABSTRACT:
In a device for breaking up ice formed on a contoured surface before it reaches a dangerous thickness, a flexible and porous membrane is fixed on the contoured surface along airtight lines of contact defining elementary chambers, each of which communicates with a main chamber inside the contoured surface. The main chamber is fed continuously by a source of hot gases. The closing up of the pores of the membrane by ice causes an inflation of the elementary chambers and a deformation of the membrane. Application is to the cowl of the air intake of a turbojet engine and to a detector used for the control of a de-icing device of any type.

REFERENCES:
patent: 2168328 (1939-08-01), Diehl
patent: 2489799 (1949-11-01), Minshall
patent: 2876970 (1959-03-01), Halbert
patent: 3614038 (1971-10-01), Nichols
patent: 3976270 (1976-08-01), Catchpole

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