| 摘要 |
The invention concerns a spark resistant structure, in particular for aircraft, characterised in that the external element (1) comprises, under a surface conducting coat (5), an electrically conducting strip (20) extending longitudinally in the direction (L-L) of the fixing means (14, 18) alignment, traversed by said fixing means (14) and in electric contact therewith, and the electric contact between, on one hand, each of said fixing means (14, 18) and the surface conducting coat (5) and, on the other, with the conductive strip (22), is obtained by an amount of electrically conductor paste (17) inserted in said external element (1) holes (11).
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