Conductive joint seals for composite aircraft

Stock material or miscellaneous articles – Sheet – web – or layer weakened to permit separation through...

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403 2, 403 24, 403267, 428223, 428244, 428273, 428283, 4283157, 4283177, 428408, 428415, B65D 6528

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045565929

ABSTRACT:
In a composite aircraft formed of graphite reinforced epoxy plates forming walls of the aircraft and walls of fuel tanks therein, for example, there is an adhesive seal for bonding overlapping faying plate surfaces together. The seal is formed of spaced glass fibers mixed with a conductive material and impregnated with a resin. The resin is cured between the surfaces of the plates to which it is bonded. The conductive filler is carbon in the form of approximate microspheres, generally hollow and having diameters in the range of 5 to 150 microns. The carbon microspheres function to weaken the adhesive seal between the plates so that they can be forcibly separated by a wedge without structural damage to the plates. The conductive material equalizes negative and positive static charges in the aircraft, particularly in fuel tanks, to eliminate electrical potential differences in the wall structures and in the materials therein.

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patent: 3347978 (1967-10-01), Simon et al.
patent: 3723223 (1973-03-01), Le Compte
patent: 4177352 (1979-12-01), Sunbar et al.
patent: 4312912 (1982-01-01), Tamura
patent: 4323623 (1982-04-01), Ahrens et al.

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