发明名称 Aircraft component with Electrically Conductive Nanocoating
摘要 A device has a first electrically conductive component (502; 108), a second electrically conductive component (504; 108), and an electrically conductive nanocoating (ECN) (200) electrically connecting the first electrically conductive component to the second electrically conductive component. An aircraft (100) has an engine (106), a fuselage (102), and a device having a first electrically conductive component, a second electrically conductive component, and an electrically conductive nanocoating (ECN) (200) electrically connecting the first electrically conductive component to the second electrically conductive component. A method (600) of providing an electrical conduction path includes providing a first electrically conductive component (502; 108), providing a second electrically conductive component (504; 108), and decreasing an electrical resistance between the first electrically conductive component and the second electrically conductive component using an electrically conductive nanocoating (ECN).
申请公布号 EP2774960(A1) 申请公布日期 2014.09.10
申请号 EP20130165369 申请日期 2013.04.25
申请人 BELL HELICOPTER TEXTRON INC. 发明人 SOTTIAUX, DANIEL P;DAVIS, HUNTER
分类号 C09D5/24;B64C27/35;B64D45/02;H01B5/14;H05K9/00 主分类号 C09D5/24
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