公开(公告)号：US20200346771A1

公开(公告)日：2020-11-05

申请号：US16807351

申请日：2020-03-03

Applicant: Airbus Operations SAS

Inventor： Thomas DEFORET ,  Rémi LANSIAUX ,  Olivier DUBOIS ,  Anthony MERTES ,  David ALRIC ,  Stéphane NOGUES

IPC: B64D27/26

Abstract: A linking device connecting an aircraft engine and a primary structure of an aircraft pylon, comprising a support connected to the primary structure, a spreader, extending between first and second ends that has a central part connected to the support by a principal link comprising a principal rotation axis, at least one system for limiting the deflection of the spreader comprising an extension secured to the spreader and also upper and lower stops, secured to a fitting secured to the support, between which the extension is positioned.