| 摘要 |
Lightning protection system (1) for aircraft structures, comprising a fastening element (4) for attaching an internal structure (63) to an external structure (62), and a composite material providing lightning protection to areas surrounding the fastening element (4), the lightning protection 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. |
