Patent ID: 8534597

Claim:
A propulsion assembly for an aircraft, comprising: a turbojet engine comprising a fan casing and an engine casing; a pylon for supporting the turbojet engine; and a device for suspending the turbojet engine beneath the pylon comprising: front suspension connecting rods extending between said fan casing and said pylon in a plane substantially perpendicular to an axis of said turbojet engine, rear suspension connecting rods extending between a rear portion of said engine casing and said pylon in a plane substantially perpendicular to the axis of said turbojet engine, said rear suspension connecting rods being substantially parallel with one another a thrust-absorbing connecting rod extending between a front portion of said engine casing and said pylon in a plane comprising the axis of said turbojet engine, and an additional connecting rod extending between said fan casing and said pylon in a direction substantially parallel to that of the axis of said turbojet engine.