MOUNTING SYSTEM INSERTED BETWEEN AN AIRCRAFT ENGINE AND A RIGID STRUCTURE OF AN ATTACHMENT STRUT FIXED UNDER A WING OF THIS AIRCRAFT

摘要

This invention relates to a mounting system(1) inserted between an aircraft engine and a rigidstructure of a strut, comprising a thrust resistancedevice (20) comprising a spreader beam (28) providedwith two lateral lower ends (32a) placed such that ahorizontal plane passes through them and through alongitudinal axis of the engine. Moreover, the device(20) is also fitted with two fittings (44) eachcomprising a forward end (44a) through which the saidhorizontal plane also passes and fixed to a forwardpart of a central casing (22), and an aft end (44b)connected to one of the ends (32a). Furthermore, thespreader beam is connected to the forward mount and tothe rigid structure through its upper end (30b).