H - Electricity – 05 – F
Patent
H - Electricity
05
F
317/3.4
H05F 3/00 (2006.01) B64D 45/02 (2006.01)
Patent
CA 1098956
Docket 6394 AIRCRAFT STATIC DISCHARGER Abstract of the Disclosure A static discharger for use on aircraft includes an elongated nylon body, and an internal resistance element is in the form of a fiber glass rod having conductive coating thereon received within an elongated opening formed in the body. The remote end of the conductive rod is mechanically and electrically bonded to a transversely oriented tungsten corona discharge needle r while the inner end of the rod is mechanically and electrically connected to a mounting base portion through a spring arrangement by means of which the differences in thermal coefficients of expansion between the body and the rod are accommodated. In one embodiment a stainless steel coil spring is used, and in another embodiment, the spring takes the form of a block of conductive rubber. A lighting diverter strip is formed along an outside surface of the nylon body.
293068
Dayton-Granger Aviation Inc.
Gowling Lafleur Henderson Llp
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