LINKING DEVICE CONNECTING AN ENGINE OF AN AIRCRAFT AND A PRIMARY STRUCTURE OF AN AIRCRAFT MAST COMPRISING A RUDDER AND A SYSTEM FOR LIMITING THE OUT-OF-PLANE DISPLACEMENT OF THE RUDDER, AIRCRAFT COMPRISING SUCH A LINKING DEVICE

摘要

The invention relates to a connecting device connecting an aircraft engine and a primary structure of an aircraft mast, comprising: - a support (54) connected to the primary structure, - a lifter (58), s 'extending between first and second ends (58.1, 58.2) which has a central part (58.3) connected to the support (54) by a main link (60) comprising a main axis of rotation (66), - at least one system of limitation (80) of the travel of the beam (58) comprising an extension (82) integral with the beam (58) and upper and lower stops (84, 86), integral with a fitting (74, 74 ') integral with the support (54), between which the extension (82) is positioned.