Pylon for attaching an aircraft turbine engine comprising aligned front wing ties

A pylon (4) for attaching a turbine engine for an aircraft, said pylon having a rigid structure (10) and means for attaching the pylon on a wing of the aircraft, said means for attaching the pylon on the wing comprising two side front ties (11a, 11b) each designed so as to take thrust forces exerted along a longitudinal direction (X) of the pylon, each side front tie comprising a fitting (54) pierced with a first orifice (65) and intended to be firmly attached to one of the elements taken from the rigid structure (10) and the wing, as well as a yoke (66) intended to be firmly attached to the other one of these elements, and a joint member (68) connecting said fitting (54) and the yoke (66) by crossing said first orifice (65), said attachment means further including a central front tie (15) designed so as to take the forces exerted along a transverse direction (Y) of the pylon,

• characterized in that said central front tie (15) comprises a ball joint (27), and is laid out between both of the side front ties (11a, 11b) so that the centre (72) of the ball joint is located, as seen along the transverse direction (Y), in each of the first two orifices (65) of the side front ties.