公开(公告)号：US10647441B2

公开(公告)日：2020-05-12

申请号：US16192950

申请日：2018-11-16

Applicant: Airbus Operations SAS

Inventor： Stéphane Combes ,  Jean Geliot ,  Thomas Deforet ,  Adeline Soulie ,  Benoit Orteu

IPC: F16M13/00 ,  B64D27/26 ,  F02C7/20

Abstract: A rear engine attachment for an engine of an aircraft which comprises a pylon having a bottom face, the rear engine attachment comprising a first fitting configured to be fixed against the bottom face and having a wall, a second fitting configured to be secured to a structural casing of the engine, two front links and two rear links, which are fixed by one and the same main link point to the wall and by two link points on either side of the second fitting. Such a motorization assembly allows for a reduction of the bulk, in particular at the rear engine attachment, which helps in improving the overall performance of the motorization assembly.