Electric charge dissipation system for aircraft

    公开(公告)号:US10513347B2

    公开(公告)日:2019-12-24

    申请号:US15828447

    申请日:2017-12-01

    Abstract: A method and apparatus comprising a first composite layer and a second composite layer in which the second composite layer is associated with the first composite layer. The first composite layer and the second composite layer form a structure. The second composite layer has a conductivity configured to dissipate an electric charge on a surface of the structure and limit a flow of an electrical current in the second composite layer in which the electrical current is caused by an electromagnetic event.

    ELECTRIC CHARGE DISSIPATION SYSTEM FOR AIRCRAFT

    公开(公告)号:US20180086479A1

    公开(公告)日:2018-03-29

    申请号:US15828447

    申请日:2017-12-01

    CPC classification number: B64D45/02 B64D37/32 Y02T50/44

    Abstract: A method and apparatus comprising a first composite layer and a second composite layer in which the second composite layer is associated with the first composite layer. The first composite layer and the second composite layer form a structure. The second composite layer has a conductivity configured to dissipate an electric charge on a surface of the structure and limit a flow of an electrical current in the second composite layer in which the electrical current is caused by an electromagnetic event.

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