Spark resistant structure, in particular for aircraft

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 45/02 (2006.01)

Patent

CA 2285102

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).

Selon l'invention, l'élément externe (1) comporte, sous une couche superficielle conductrice (5), une bande électriquement conductrice (20) s'étendant longitudinalement dans la direction (L-L) de l'alignement des moyens de fixation (14, 18), traversée par lesdits moyens de fixation (14) et en contact électrique avec eux, et le contact électrique entre chacun desdits moyens de fixation (14, 18), d'une part, et la couche superficielle conductrice (5) et ladite bande conductrice (22), d'autre part, est obtenu au moyen d'une dose de pâte électriquement conductrice (17) introduite dans les trous (11) dudit élément externe (1).

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