Patent ID: 7909285

Claim:
A suspension for suspending a turbine engine from the structure of an aircraft, comprising: a beam, the beam including a first element including a first attachment unit which attaches the beam to said structure, a second element including a second attachment unit which attaches the beam to the turbine engine, a first plate attached to the first element, the first plate being positioned transverse to an axis of the engine, a second plate attached to the second element, the second plate being positioned transverse to the axis of the engine, and a layer of a flexible and damping material positioned transverse to the axis of the engine and sandwiched between the first plate and the second plate, wherein a first face of the layer of the flexible and damping material abuts a first face of the first plate and a second face of the layer of the flexible and damping material, opposite the first face, abuts a first face of the second plate, and wherein the second attachment unit includes at least one link rod articulated by a ball joint to the second element of the beam.