Pneumatic deicer for shedding thin ice

Aeronautics and astronautics – Aircraft structure – Ice prevention

Patent

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Details

B64D 1518

Patent

active

051120119

ABSTRACT:
An inflatable deicer having deicing tubes formed by adjacent rows of stitching between inner and outer plies with a manifold tube intersecting and extending across the deicing tubes. The stitching of the deicing tubes is turned at the edges of the manifold to reinforce the edges of the manifold tube. The deicing tubes are narrow and the inflation pressure is high for a short activation time at relatively long intervals to shed thin ice.

REFERENCES:
patent: 2957662 (1956-02-01), Hess
patent: 3370814 (1968-02-01), Kageorge et al.
patent: 3690601 (1972-09-01), Roemke
patent: 4516745 (1985-05-01), Ely
patent: 4561613 (1985-12-01), Weisend
patent: 4836474 (1989-06-01), Briscoe et al.
Dwight L. Loughborough, Howard E. Greene, Paul A. Roush, "A Study of Wing De-Icer Performance on Mount Washington", Sep. 1948, vol. 7, No. 9.

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