Multiple port connection pneumatic deicing system

Aeronautics and astronautics – Aircraft structure – Ice prevention

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244134R, B64D 1516

Patent

active

052753620

ABSTRACT:
A pneumatic deicing system includes a deicer assembly 32 comprised of an outer ply 52, an inner ply 54, and a plurality of inflatable tube-like members 36 provided therebetween. The deicer assembly is disposed directly on top of and bonded to the airfoil 34. Pressurized fluid is provided to the tube-like members via a manifold 40 in the deicer assembly which is positioned directly over a plurality of ducts 42 provided through the airfoil.

REFERENCES:
patent: 2436889 (1948-03-01), Heston
patent: 2489799 (1949-11-01), Minshall
patent: 2515519 (1950-07-01), Lawrence et al.
patent: 2957662 (1960-10-01), Hess
patent: 4516745 (1985-05-01), Ely et al.
patent: 4561613 (1985-12-01), Weisend, Jr.
patent: 4613102 (1986-09-01), Kageorge
patent: 5112011 (1992-05-01), Weisend, Jr. et al.

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