Aircraft engine assembly comprising at least two rear engine attachments axially shifted from each other

An aircraft engine assembly comprising:

• a dual-body engine comprising an inter-turbine casing;
• a pylon for mounting the engine on a structure of the aircraft, the pylon including a primary structure;
• a mount for mounting the engine on the primary structure of the mounting pylon;
• the mount comprising a rear engine attachment assembly comprising:
• a first connecting rod articulated at one end with a bracket rigidly connected to the inter-turbine casing and articulated at another end with a bracket rigidly connected to the primary structure of the pylon, the first connecting rod being arranged in a median vertical and longitudinal plane;
• a second connecting rod articulated at one end with a bracket rigidly connected to the inter-turbine casing and articulated at another end with a bracket rigidly connected to the primary structure of the pylon, the second connecting rod being arranged substantially tangential to the inter-turbine casing;
• and
• a rear engine attachment for transverse force spreading, shifted axially backwards in relation to the first and second connecting rods, and including a shear pin oriented in a vertical direction of the engine assembly and rigidly connected to either the engine or the primary structure, as well as a seating bracket for the shear pin that is rigidly connected to another of the engine or the primary structure and that has a seating orifice for the shear pin, the shear pin being seated in the seating orifice with a clearance in the longitudinal direction of the engine assembly.