AIRCRAFT ENGINE MOUNTING STRUCTURE INCLUDING A REAR ENGINE ANCHOR BEAM LOCATED AT A DISTANCE FROM THE STRUCTURE BOX

摘要

The invention relates to an aircraft engine mounting structure including an intermediate part (120) disposed between a crossbar supporting element (100) and a rigid structure box (10), a first shearing pin (124) extending through a first securing interface plane (Pi1) between the part (120) and the structure box and a second shearing pin (126) extending through a second securing interface plane (Pi2) between the part (120) and the supporting element (100). In addition, in side elevation, the point of intersection (Q1) between an axis (125) of the pin (124) and the plane (Pi1) and the point of intersection (Q2) between an axis (127) of the pin (126) and the plane (Pi2) are located on the common axis (130) of two lateral thrust-absorbing link rods (90) hinged to the crossbar (92).