公开(公告)号：US10858114B2

公开(公告)日：2020-12-08

申请号：US16431280

申请日：2019-06-04

Applicant: Airbus Operations SAS

Inventor： Thomas Deforet ,  Jacky Puech

IPC: F16M11/00 ,  B64D27/26

Abstract: An assembly for an aircraft comprising a pylon having a mounting plate having a front face and a rear face and through which there passes, between the front face and the rear face, at least one central bore, a front engine mount comprising a spar with a rear face bearing against the mounting plate front face and which, for each central bore, has a complementary central bore aligned with the central bore, and for each central bore, a mounting system. The mounting system comprises a shear pin inserted into the central bore and the complementary central bore from the rear face with a flange bearing against the rear face, a support with a central hole, the diameter of which is greater than the flange diameter and fixed to the rear face, and a cap fixed to the support closing off the central hole and bearing against the shear pin.