Linking device more specifically suited to providing the link between an air intake and an engine of an aircraft nacelle

摘要

The nacelle has two conduits connected together by a fastening device, which comprises two annular flanges (46, 50) respectively attached to an air inlet (42) and an engine (44). A fastening element (56) i.e. bolt, has rods (58) housed in respective passage holes (54). An angle profile (66) is inserted between the fastening element and a cylindrical portion (57) adjacent to one of the flanges. The profile is connected to the cylindrical portion through an intermediary of another fastening element (68), which comprises an absorbing unit absorbing eventual deformations along radial direction.