Integral lightning protection system for composite aircraft skin

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

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244 1A, H05F 102

Patent

active

045020922

ABSTRACT:
Method and structures for enhancing the conductivity of graphite composite materials for lightning protection and prevention of attachment of lightning to fasteners. The integral lightning protection for composite aircraft skins, including skins with fasteners penetrating into fuel tanks, utilizes metal coated or plated graphite fibers which are woven into the outer layer of tape or fabric of the structural component requiring protection.

REFERENCES:
patent: 2982494 (1961-05-01), Amason
patent: 3568311 (1971-03-01), Lawton
patent: 3755713 (1973-08-01), Paszkowski
patent: 3879638 (1975-04-01), Day
patent: 3989984 (1976-11-01), Amason et al.
patent: 4382049 (1983-05-01), Hofmeister et al.

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