Electro-impulse deicing system

Details Electro-impulse deicing system Electro-impulse deicing system

B - Operations, Transporting

64

D

244/105

B64D 15/16 (2006.01)

Patent

CA 1241317

ABSTRACT What is proposed is an electro-impulse de-icing device for use in an airfoil of an aircraft that includes a system having an energy storage device connected via a triggering device to a set of coils, each embodying a coil construction in the form of a spirally-wound ribbon coil, whose planar dimension is pressed against an interior surface in the leading edge of the airfoil, and wherein the coil sets are arranged in a linear manner along the long axis of the airfoil and are energized simultaneously and sequentially via an interlocking pattern from the wing tips or from the fuselage of the aircraft with each coil set being triggered twice from about three to five seconds apart.

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