发明名称 Aeronautical static discharge device and indicator therein
摘要 A static discharge device includes a body an an electrical path carried in the body for discharging static electricity. Carried on the body is visual indicia indicating a present operational status of the electrical path to discharge static electricity effectively. The visual indicia is observable to an airplane operator or technician to quickly determine the operational or non-operational status of the static discharge device.
申请公布号 US9346559(B1) 申请公布日期 2016.05.24
申请号 US201514833117 申请日期 2015.08.23
申请人 Skelton Grady L. 发明人 Skelton Grady L.
分类号 B64D45/02;G08B5/36 主分类号 B64D45/02
代理机构 Thomas W. Galvani, P.C. 代理人 Thomas W. Galvani, P.C. ;Galvani Thomas W.
主权项 1. A static wick for shedding electricity from an airplane, the static wick comprising: a body; an electrical path through the body from a base to a discharge end, the electrical path including a spiral-wound conductive element; and observable, visual indicia carried by the body indicating a present operational status of the electrical path, the visual indicia being responsive to provision of heat to the visual indicia from the spiral-wound conductive element; wherein the spiral-wound conductive element produces heat in response to degradation of the electrical path and provides said heat to the visual indicia.
地址 Queen Creek AZ US