Propulsion assembly for aircraft comprising a turbojet engine, a pylon and means for mounting the turbojet engine on the pylon

A propulsion assembly of an aircraft, said propulsion assembly having a longitudinal axis and a vertical median plane passing through the longitudinal axis, and the propulsion assembly comprising:

• a turbojet engine comprising a front casing extending between a front face and a rear face perpendicular to the longitudinal axis and a rear casing, wherein the longitudinal axis comprises an axis of rotation of the turbojet engine;
• a mounting pylon having a primary structure with a front wall;
• an engine mount comprising a first connecting rod and a second connecting rod which are arranged, respectively, on each side of the median plane, wherein one of the first and second connecting rods is mounted in an articulated manner by a first connecting point on the front wall and by a second connecting point on the front casing, wherein the other of the first and second connecting rods is mounted in an articulated manner by a third connecting point and a fourth connecting point on the front wall and by a fifth connecting point on the front casing, and wherein the first connecting point, the second connecting point, the third connecting point, the fourth connecting point, and the fifth connecting point are in a front third of the front casing;
• connecting rods mounted in an articulated manner between the mounting pylon and the turbojet engine;
• two external connecting rods arranged, respectively, on both sides of the median plane, wherein each external connecting rod has a rear end mounted in an articulated manner on a lower spar of the primary structure by a first rear connecting point and a front end mounted in an articulated manner on the rear face by a first front connecting point;
• and
• two internal connecting rods arranged, respectively, on both sides of the median plane, wherein each internal connecting rod has a rear end mounted in an articulated manner on the lower spar by a second rear connecting point and a front end mounted in an articulated manner on the rear face or on the rear casing by a second front connecting point, and wherein axes of the two internal connecting rods converge toward the longitudinal axis.