Patent ID: 7121504

Claim:
A hanging device connecting an engine to an aircraft wing, said device comprising a rigid structure and hanging equipment interposed between said rigid structure and the wing, said hanging equipment comprising: a forward attachment and a rear attachment including at least one triangular shackle placed in a vertical plane aligned along a transverse direction (Y) of the aircraft, said forward attachment being formed of two half-attachments arranged respectively on one side and the other of a vertical plane passing through a longitudinal axis of the engine, wherein each half-attachment comprises at least one triangular shackle placed in a vertical plane aligned along a longitudinal direction (X) of the aircraft, and so that said hanging equipment is made up exclusively of said forward and rear attachments; wherein the rear attachment is made up of a pair of triangular shackles placed in vertical planes aligned along the transverse direction (Y) of the aircraft, and wherein the forward attachment is made up, on one side and the other of the vertical plane passing through the longitudinal axis of the engine, of a pair of triangular shackles placed in vertical planes aligned along the longitudinal direction (X) of the aircraft; and wherein said rear attachment comprises a bracket integral with the rigid structure, connected to said pair of shackles by at last one pin aligned in the longitudinal direction (X) of the aircraft, and wherein said rear attachment further comprises a bracket integral with the wing, connected to said pair of triangular shackles by at least one pin aligned in the longitudinal direction (X) of the aircraft.