Aeronautics and astronautics – Aircraft structure – Ice prevention
Patent
1997-02-24
1998-09-29
Grant, William
Aeronautics and astronautics
Aircraft structure
Ice prevention
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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Butler Donald E.
Fahrner Alan J.
Rauckhorst, III Richard L.
Waples Thomas A.
Grant William
Romanchik Richard A.
The B. F. Goodrich Company
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