Hinge for a door of an aircraft, with passage for a cable
OwnerBenjamin Boisnierinventor
Life of this patent
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Abstract
A hinge to open or to close a door, for example a door of an electrical cabinet of an aircraft, including at least one first wall and one second wall defining an angular opening of the hinge and a hollow internal space of the hinge sized to receive a cable. The first wall and the second wall are positioned relative to one another in order to open the hinge in a cable insertion or extraction position to allow the cable to pass through the angular opening of the hinge inside or outside the internal space, and to close the hinge in working positions of the hinge between a maximum open position of the door and a closed position of the door to block the angular opening of the hinge so as to be able to enclose the cable in the hollow space.
Claims9
A hinge to open or to close a door or a door of an electrical cabinet of an aircraft, including at least one first wall and one second wall defining an angular opening of the hinge and a hollow internal space of the hinge sized to receive a cable, the first wall and the second wall being positioned relative to one another in order:
- to open the hinge in a cable insertion or extraction position to allow the cable to pass through the angular opening of the hinge inside or outside the internal space;
- and
- to close the hinge in working positions of the hinge between a maximum open position of the door and a closed position of the door to block the angular opening of the hinge so as to be able to enclose the cable in the hollow space.
Dependencies are inferred from the claim text.