AIRCRAFT ENGINE ATTACHMENT DEVICE COMPRISING TWO THRUST-REACTING LINK RODS THAT FIT TOGETHER TRANSVERSELY

摘要

The present invention relates to an aircraft engine attachment device comprising a rigid structure and means for attaching the engine to the rigid structure, the attachment means comprising a thrust-reacting device (14) comprising two lateral thrust-reacting link rods (26) each having a rear end (26b) mounted on a balance beam (28) of the device (14) via a mechanical link (44). According to the invention, each link (44) is made using a peg (48) provided on the balance beam and passing through a hole (50) made in the rear end (26b), the peg (48) being arranged in such a way as to run substantially transversely with respect to the attachment device.