Patent ID: 8733689

Claim:
A device for providing electrical continuity between aeronautical components with relative movement, applicable in aeronautical structures including at least a first fixed component ( 1 ) and a second component ( 2 ) displaceable with respect to the first component ( 1 ), each of the first component ( 1 ) and the second component ( 2 ) being provided with an electrically conductive surface; wherein said device includes at least a first conductive piece fixed to the first component ( 1 ) and a second conductive piece fixed to the second component ( 2 ) displaceable with respect to the first component, the first piece and the second piece being joined together with the possibility of sliding one over the other; and the first piece being connected to the conductive surface of the first component ( 1 ) and the second piece being connected to the conductive surface of the second component ( 2 ), so that when the second component is displaced with respect to the first component, sliding selected between a sliding of the first piece over the second piece and sliding of the second piece over the first piece, takes place, maintaining the electrical conductivity between the first ( 1 ) and second ( 2 ) components, wherein the second piece is arranged in an area in which the distance between the second component ( 2 ) and the first component ( 1 ) varies in at least one area of the trajectory followed by the second component ( 2 ) on the first component ( 1 ); and said second piece having a configuration equivalent to said trajectory; the first piece comprising a telescopic arm provided with a mooring and sliding skid ( 10 ) on the configuration of the second piece ( 2 ) equivalent to the trajectory followed by the second component ( 2 ) on the first component ( 1 ).