Safran Aircraft Engines

Eric Francois Michel Maingre

Guillaume Glemarec

Jean-Baptiste Vignes

The invention relates to an assembly between an aircraft pylon () and a turbomachine () of longitudinal axis (X), the pylon () and the turbomachine () each comprising front and rear longitudinal regions, the assembly comprising a rear support () configured to connect the rear region of the turbomachine () to the rear region of the pylon (), the assembly being characterized in that the rear support () comprises a sliding pivot connection arranged between the rear region of the turbomachine () and the rear region of the pylon (), so as to allow the turbomachine () only translational and rotational movements along and about the longitudinal axis (X) and along and about a vertical axis (Z) and a rotational movement about a transverse axis (Y).

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Moissy-Cramayel, France

Eric Francois Michel Maingre