Pneumatic de-icer having improved aerodynamic characteristics

Aeronautics and astronautics – Aircraft structure – Ice prevention

Patent

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B64D 1516

Patent

active

054491339

ABSTRACT:
A de-icer for attachment to an airfoil subject to impingement by an airstream. The airstream induces a stagnation line near the leading edge of the airfoil. The de-icer has inflatable passages that are parallel to the airstream overlying the airfoil on one side of the stagnation line, and inflatable passages that are parallel to the leading edge overlying the airfoil on the other side of the stagnation line. The de-icer maintains the aerodynamic characteristics of the airfoil during de-icer inflation. A method of manufacturing the de-icer is also provided.

REFERENCES:
patent: 2436889 (1948-03-01), Hester
patent: 2957662 (1960-10-01), Hess
patent: 3370814 (1968-02-01), Kageorge
patent: 3604666 (1971-09-01), Achberger
patent: 4516745 (1985-05-01), Ely et al.
patent: 4561613 (1985-12-01), Weisend, Jr.
patent: 4779823 (1988-10-01), Ely et al.
patent: 5074497 (1991-12-01), Phillips, II

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