Flush precipitation static discharger system for aircraft

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

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244 1A, 361222, E05F 300

Patent

active

043982344

ABSTRACT:
A flush, zero drag discharger system for dissipating static electric charges from surfaces of high performance aircraft and similar vehicles which is capable of withstanding a severe lightning environment without substantial degradation of the system. The discharger system includes a configuration of the vehicle secondary structure into non-electrically conductive areas, conductive high corona threshold areas, and controlled low corona threshold electrostatic discharge areas which are protected from the detrimental effects of lightning by the utilization of ionization-type lightning diverters.

REFERENCES:
patent: 1419261 (1922-06-01), Howard
patent: 2933732 (1960-04-01), Tanner
patent: 3906308 (1975-09-01), Amason et al.
patent: 4237514 (1980-12-01), Cline

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