| 摘要 |
Lightning protection system (1) for aircraft structures comprising a composite material, for providing lightning protection to areas surrounding a fastening element (4), the fastening element (4) attaching an internal structure (63) to an external structure (62), the system (1) comprising at least one conductive layer (2, 3) embedded in the matrix of said composite material and in proximity to the fastening element (4), the conductive layer (2, 3) comprising conductive nanoparticles dispersed within its structure. |
