Composite aircraft structure having lightning protection

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

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361117, H05F 300

Patent

active

043521428

ABSTRACT:
A lightning protection system for advanced composite aircraft structures consisting of a sandwich structure including two layers of aluminum foil separated by a layer of dielectric material. The sandwich structure is applied to the surface of the composite aircraft structure desired to be protected from lightning strike damage thereby confining damage to the sandwich structure which can be removed and replaced.

REFERENCES:
patent: 3480231 (1967-11-01), Lumn
patent: 3482802 (1969-12-01), Lumn
patent: 3498572 (1970-03-01), Lumn
patent: 3906308 (1975-09-01), Amason et al.
patent: 3989984 (1976-11-01), Amason et al.

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