Electro-expulsive separation system

Aeronautics and astronautics – Aircraft structure – Ice prevention

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318116, B64D 1500

Patent

active

046903534

ABSTRACT:
An electro-expulsive system 20 has one or more overlapped conductors OC1-OCN each comprising a flexible ribbon conductor 32 which is folded back on itself. The conductors are embedded in an elastomeric material 33. Large current pulses are fed to the conductors OC1-OCN from power storage units 1-N. As a result of the antiparallel currents I and I', the opposed segments of a conductor 32 are forcefully separated and the elastomeric material is distended. Void 34 in the elastomer aids the separation of the conductor segments. The distention is almost instantaneous when a current pulse reaches the conductor and the distention tends to remove any solid body on the surface of the elastomeric material.

REFERENCES:
patent: 3672610 (1972-06-01), Levin
patent: 3809341 (1974-05-01), Levin
patent: 4494715 (1985-01-01), Weisend, Jr.
patent: 4545553 (1985-10-01), Finke

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