Aircraft lightning strike protection and grounding technique

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane and cylindrical rotor sustained

Reexamination Certificate

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C244S119000, C244S123800

Reexamination Certificate

active

07014143

ABSTRACT:
An aircraft panel assembly10is provided, including a panel core28,a plurality of pre-preg layers30surrounding the panel core28forming an internal layer of plies34,at least one metal foil layer38positioned on an outer layer40of the internal layer of plies34.The at least one metal foil layer38providing an electrical conduit between the outer surface24of the aircraft panel assembly10and a sub-structure26for grounding.

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patent: 0 783 960 (1997-07-01), None
patent: 2 626 629 (1989-08-01), None
Lightning Strike Products, Sep. 2002, XP-002270680.

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