公开(公告)号：US20220340293A1

公开(公告)日：2022-10-27

申请号：US17725641

申请日：2022-04-21

Applicant: Airbus Operations SAS

Inventor： Michael BERJOT ,  Rémi LANSIAUX ,  William BRAS ,  Germain GUENEAU ,  Sébastien VAN ARENDONK ,  Jacques DEMANGE ,  Sébastien COMMENGE

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 having a central part connected to the support and a first and a second end that are connected to thrust rods, at least one limiting system for limiting the travel of the spreader having an upper and a lower stop between which is positioned the first or second end of the spreader, the upper and the lower stop being connected to one another so as to form a single part connected to a fitting secured to the support.