REAR SECTION OF AN AIRCRAFT INCLUDING AN ENGINE MOUNTING STRUCTURE SWINGABLY MOUNTED ON THE FUSELAGE

摘要

The invention relates to a rear section of an aircraft including two connecting rods (66) symmetrically arranged on either side of a vertical median plane (P), each connecting rod having an end mounted on an engine mounting structure (14) and another end mounted on the fuselage (6), said section being designed so as to enable, by rotating the connecting rods (66) about the rotational axes thereof, a limited amplitude swinging movement of the assembly (23) formed by the mounting structure and the engines, relative to the fuselage (6), through first and second openings (18) of the fuselage.