SET INCLUDING AN AIRCRAFT TURBOMACHINE AND ITS MOUNTING PYLONE

Abstract

Assembly (201) comprising a turbomachine (203) and a tower (205), the turbomachine (203) extending longitudinally along an axis (X) and comprising, from upstream to downstream, a propeller (207), an upstream casing (209), an intermediate casing (211), a body (213) and a downstream casing (215), as well as, in a plane (P1), a first suspension member (217) connected to the tower and the upstream casing, in a plane (P2), a second suspension member (219) connected to the tower and the intermediate casing, and, in a plane (P3), a third suspension member (221) connected to the tower and the downstream casing, the third suspension member comprising a monobloc connecting element extending in the plane (P3) and having a first arm fixed to the tower and extending radially towards the downstream casing along a associated extension direction, and the second and third branches extending on either side of the first branch in the plane (P3) according to an associated extension direction and connected to the downstream casing,the first, second and third branches being arranged so as to deform in the plane (P3) along a direction perpendicular to their associated extension direction. Figure for the abbreviation: [Fig.2],

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