Patent ID: 8814079

Claim:
An attachment pylon to attach a turbine engine to a wing of an aircraft, comprising: a rigid structure including a first protruding fitting and a second protruding fitting, each of the first protruding fitting and the second protruding fitting having a first orifice; an attaching member to attach the pylon onto the wing, the attaching member including a first side front tie and a second side front tie, each of the first side front tie and the second side front tie being configured to take thrust forces exerted along a longitudinal axis of the pylon, the first side front tie being secured to the first orifice of the first protruding fitting, and the second side front tie being secured to the second protruding fitting; and a first joint member connecting the first protruding fitting and the first side front tie by crossing the orifice of the first protruding fitting, and a second joint member connecting the second protruding fitting and the second side front tie by crossing the orifice of the second protruding fitting, wherein the attaching member further includes a central front tie configured to take forces exerted along a transverse axis of the pylon, the central front tie including a ball joint laid out between the first side front tie and the second side front tie so that a center of the ball joint is aligned with at least a portion of the orifice of the first protruding fitting and at least a portion of the orifice of the second protruding fitting along the transverse axis of the pylon.