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 |