Pneumatic deicing system with drain valve

Aeronautics and astronautics – Aircraft structure – Ice prevention

Patent

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Details

244134E, 220339, 215237, B64D 1518

Patent

active

058136312

ABSTRACT:
A pneumatic deicing system includes a deicer assembly comprised of an outer layer, an inner ply, and a plurality of inflatable members provided therebetween. The deicer assembly is disposed directly on top of and bonded to an airfoil. The deicer assembly is inflated through an inflation port. Fluid is drained from the deicer assembly through a drain valve.

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patent: 5489073 (1996-02-01), Leffel et al.
patent: 5577688 (1996-11-01), Sloan

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