Aeronautics and astronautics – Aircraft structure – Ice prevention
Patent
1983-06-09
1985-04-02
Blix, Trygve M.
Aeronautics and astronautics
Aircraft structure
Ice prevention
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
Cattaneo Christian J.
Derouet Patrick R. J.
Laroche Michel C. F.
Blix Trygve M.
Corl Rodney
S.N.E.C.M.A.
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