REAR PART OF AN AIRCRAFT COMPRISING A STRUCTURE FOR SUPPORTING ENGINES, CONNECTED TO THE FUSELAGE BY AT LEAST ONE BLOCKING ELEMENT UNDER COMPRESSION LOADING

摘要

The invention relates to an aircraft rear portion (1) comprising an engine support structure (14) passing through the fuselage at first and second openings (18, 18). It has attachment means connecting the support structure (14) to the fuselage (6), comprising first attachment means connecting the structure (14) to a first frame (50) forming the first opening and second means fastener connecting the structure (14) to a second frame (50) forming the second opening. According to the invention, the first and second attachment means each comprise at least one locking element (90, 92) of said support structure, biased in compression while being supported on the one hand on the frame (50). , and secondly on the support structure (14).