ROPE RESTRAINT DEVICE FOR AN AIRCRAFT ENGINE HITCHING MACHINE, INTEGRATING THREE ALIGNED ROTORS

摘要

The present invention relates to a device for taking up the thrust forces (14) for an aircraft engine mounting pylon (4), comprising a first fitting (194) integral with a rigid structure (108) of the engine mast. hooking, and two lateral rods (14a) for resumption of thrust forces. It further comprises an axle system (190) carrying three first ball members (192a, 196a) arranged along the same and belonging respectively to a primary ball joint (192) and two secondary ball joints (196) arranged from and other of the primary ball joint, the first fitting (194) integrating a second ball member (192b) cooperating with the first member (192a) of the primary ball joint (192), and one end of each of the two connecting rods (14a). ) integrating a second ball member (196b) cooperating respectively with the first members (196a) of the two secondary ball joints (196).