ELECTRIC CHARGE DISSIPATION SYSTEM FOR AIRCRAFT

摘要

A method and apparatus comprising a first composite layer (318) and a second composite layer (320) 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 (302). The second composite layer has a conductivity configured to dissipate an electric charge (310) on a surface (312) of the structure and limit a flow of an electrical current (311) in the second composite layer in which the electrical current is caused by an electromagnetic event (315).