Fastening device particularly suitable for the fastening between an air intake and an engine of an aircraft nacelle

An aircraft nacelle comprising:

• a first conduit for an air inlet;
• a second conduit for an engine;
• and
• a fastening device;
• wherein the first and second conduits are arranged end to end and connected by the fastening device;
• wherein the fastening device comprises:
• a first annular flange attached to the air inlet;
• a second annular flange attached to the engine;
• wherein, said first and second annular flanges comprise a first and a second pluralities of passage holes, defined in the annular flanges and arranged in line with each other, and
• first fastening elements comprising a plurality of rods housed in the passage holes,
• wherein, for at least one first fastening element, the passage hole of one of the first and second annular flanges has a diameter greater than the diameter of one of the plurality of rods, allowing said one rod to move in case of deformation of one of the first and second conduits and the passage hole of the other of the first and second annular flanges has a diameter adapted to the diameter of the one rod,
• wherein an angle profile is inserted between the first fastening element and a cylindrical portion adjacent to said first annular flange,
• wherein said angle profile is connected to the adjacent cylindrical portion through the intermediary of at least one second fastening element comprising a means for absorbing eventual deformations in a radial direction,
• wherein the second fastening element further comprises a deformable element inserted entirely between the angle profile and a shoulder solidly attached to said second fastening element.