Patent ID: 7907382

Claim:
An integrated device ( 1 ) for the protection against electrical discharges of conductive fixing elements ( 2 ) between one another or of a fixing element and another conductive element of an aircraft, comprising a cap ( 3 ) and an o-ring gasket ( 4 ) made of non-conductive insulating material, wherein the fixing element ( 2 ) works together with the cap ( 3 ) and the o-ring gasket ( 4 ), the fixing element ( 2 ) being surrounded by the cap ( 3 ) and the o-ring gasket ( 4 ) in a non-conductive manner, thus preventing the possibility of electrical discharges such that in the device ( 1 ) a number of necessary components is minimized, the impact in weight for the aircraft being minimum, wherein the cap ( 3 ) comprises a thread ( 11 ) for fixing the cap ( 3 ) to the fixing element ( 2 ).