Electrostatic discharger, particularly for aircrafts

Electricity: electrical systems and devices – Discharging or preventing accumulation of electric charge – Structurally combined with building or vehicle

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361222, H05F 304

Patent

active

042165199

ABSTRACT:
An electrostatic discharger has a stem of high electric resistivity faste at one end to an aircraft body and secured at its other end to an enlarged head provided with a sharp circular charge-emitting edge in a plane perpendicular to the stem axis. The edge, bounded by two annular surfaces converging at an acute angle with a radius of curvature of the order of 0.05 mm, may project radially or axially from the head and in either case has a diameter greatly exceeding that of the stem.

REFERENCES:
patent: 2536818 (1951-01-01), Lawton
patent: 3034020 (1962-05-01), Benkoczy et al.
patent: 3585447 (1971-06-01), McLain
patent: 3594611 (1971-07-01), Tanner et al.
patent: 3742300 (1973-06-01), Floyd

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