AIRCRAFT ENGINE PYLON, ASSEMBLY COMPRISING SAID PYLON AND RELATED AIRCRAFT

摘要

The invention relates to an engine (22) suspended from the linear main portion (23) of a pylon attached to an airplane fuselage or wing. The coupling comprises flat, symmetrical flanges (25a, 25b) forming an angle, for supporting a bracket (29) to which the engine (22) is connected either directly or by means of a connection element (39). The flat shape of the flanges simplifies the production thereof and provides good stress resistance. The above-mentioned intermediate connection element (39) provides good resistance to the stresses produced by the overhang of the connection. In addition, flexible links (43, 45) filter engine vibration and prevent the transmission of irregular stresses.