LATERAL TURBOJET IMPROVED IN ORDER TO LIMIT THE DEFORMATION THEREOF

摘要

The invention relates to a suspension system of a fan jet. Said fan jet comprises an intermediate housing outer rim (13) attached to the front suspension and a primary structure attached to the rear suspension. The rim and the primary structure are held in a coaxial relationship by arms (35a-35f), at least some of which are shaped and/or arranged in such a way as to be deformed in response to the thrust of the fan jet by creation of a deforming moment between the rim and the primary structure, opposing an opposite load generated by the same thrust.