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

摘要

The device (14) has a fitting (194) integrated to a rigid structure (108) of a mounting structure, where the fitting is integrated with a female ball joint unit (192b) cooperating with a ball joint unit (192). An end (14a) of connecting rods is integrated with another female ball joint unit (196b) respectively cooperating with male ball joint units (196a). Centers of the ball joint unit are aligned. Another fitting (199) is integrated to the rigid structure of the mounting structure.