A device for suspending a turboprop, then under a wing of 371

摘要

The present invention relates to a motor assembly for an aircraft comprising means for suspending a turboprop on an attachment strut, these means comprising a plurality of engine mounts before (16) each having a force transmission device of a vibration damper (20) includes a housing (22), a member of the transmission of forces (24) extending in a first axis (26) is parallel to the axis of rotation of the helix and a hollow element (28) integrated in the casing and extending in a second axis (30) is perpendicular and secant to the first axis. According to the invention, the support means of the device (20) are constituted by a plurality of lugs (32a, 32b) each having a median plane parallel to the heads of the yoke, comprising one of the first and second axes and orthogonal to the other of these axes.