Aircraft engine assembly

An aircraft engine assembly, comprising an engine, a pylon and a nacelle, in which the engine is positioned, the engine comprising:

• a core that comprises a rotor pivoting about a rotation axis, a front engine casing and a rear engine casing,
• a fan positioned in a fan casing that has an exterior radius,
• the pylon comprising a primary structure connected to the engine by an engine link that comprises:
• a rear engine mount that connects an intermediate part of the primary structure and the rear engine casing, the rear engine mount being connected to the intermediate part of the primary structure at a rear link point,
• a front engine mount that connects a front end of the primary structure and the front engine casing and that comprises at least one front rod that has at least three front link points, a first front link point configured in order to connect the front rod and the front end of the primary structure, a second front link point configured in order to connect the front rod and the core of the engine, and a third front link point configured in order to connect the front rod and the core of the engine, the second and third front link points being offset relative to one another in a horizontal direction perpendicular to the rotation axis of the engine,
• at least two thrust rods that connect the intermediate part of the primary structure and the front engine casing,
• the aircraft engine assembly being characterized in that the first front link point of the front engine mount and the rotation axis of the engine are separated by a distance greater than an exterior radius of the rear casing of the core of the engine at a rear link point of the rear engine mount, the first front link point of the front engine mount is positioned such that an upper edge of the front end of the primary structure is separated from the rotation axis of the engine by a distance smaller than the exterior radius of the fan.