Mounting device for an aircraft propulsion unit on an engine pylon

摘要

Impulsive system (10) comprises engine with central casing (16) and blower casing (20). Impulsive system is attached to fram (12) of mast with mounting mechanism comprising rear clamp (22), first front clamp (24), and second front clamp (26). Direction stress transmitted to framing of mast through second clamp has main component oriented along vertical axis OZ. An Independent claim is also included for the lock-on mast of impulsive system to part of aircraft.