| abstract |
Device for fastening an aircraft engine comprising a rigid structure and means for attaching said engine to said rigid structure, said attachment means comprising two connecting rods (26) for taking up thrust forces mechanically linked to a rudder (28), a connecting fitting (24) fastened to the rigid structure to which is attached mechanically the spreader (28) by a connecting fitting (40) by means of a connecting pin (39), an additional fitting ( 52) to which are mechanically connected the connecting rods (26), the spreader bar (28) and the connecting fitting (24), a clearance being provided at the level of the mechanical connection between the connecting rods and the additional fitting, the connection between the fitting additional (52) and the connecting fitting (24) being made by means of the connecting axis introduced laterally, orthogonally to said median plane (Pm) of the attachment device. |