发明名称 Lightning protection system for aircraft composite structure
摘要 A lightning-protected conductive composite fuel tank includes a conductive material arrayed on an outer surface to at least partially cover a fastener centerline. Through holes extend along the fastener centerline through the conductive material and the underlying fuel tank shell. These through holes are countersunk into the fuel tank shell to a depth such that a fastener in a through hole will avoid electrical continuity or communication with the conductive material on the fuel tank outer surface. The gap in the countersunk through holes, between the fastener heads and the coextensive outer surface of the fuel tank, is filled with a dielectric or nonconductive material.
申请公布号 US7969706(B2) 申请公布日期 2011.06.28
申请号 US20090573277 申请日期 2009.10.05
申请人 THE BOEING COMPANY 发明人 HEETER RUSSELL J.;MORGAN JEFFREY D.;PATE KEVIN D.;PORTER JOHN R.;HANSEN DARRIN M.;STECKMYER STEVEN C.;NGUYEN THU A.;WINTER DALE B.;SMITH DANIEL;TOWNSEND HARRY E.
分类号 H02H1/00 主分类号 H02H1/00
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