CPC B64D 27/26 (2013.01) [B64D 27/16 (2013.01); B64D 2027/262 (2013.01)] | 20 Claims |
1. Turbomachine extending along an axis, comprising a high-pressure body with a high-pressure compressor coupled in rotation to a high-pressure turbine, and a low-pressure body including a low-pressure compressor coupled in rotation to a low-pressure turbine, an upstream casing located upstream of the high-pressure compressor, and means of suspension for the turbomachine, intended for attaching the turbomachine to an aircraft pylon, the said means of suspension comprising an upstream suspension system with a beam intended to be attached to the pylon, at least two connecting rods spaced apart circumferentially from each other and each articulated at a first end to the beam and at a second end to the upstream casing, a rudder bar articulated on the beam at the level of a circumferentially central zone of said rudder bar, at least two force-recovery rods to take up the thrust forces of the turbomachine, spaced apart circumferentially from each other and each articulated at a first end on the rudder bar and at a second end on a fixed part of the turbomachine, the said at least two force-recovery rods being located upstream of a radial suspension plane defined by the two connecting rods, the means of suspension also comprising a downstream suspension system capable of connecting the pylon to a fixed downstream casing of the turbomachine.
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