公开(公告)号：US20220055758A1

公开(公告)日：2022-02-24

申请号：US17407251

申请日：2021-08-20

Applicant: Airbus Operations SAS

Inventor： Michael BERJOT ,  Thomas DEFORET ,  Jacky PUECH

IPC: B64D27/26

Abstract: A propulsion assembly including a primary structure of a pylon having right and left extensions projecting with respect to right and left lateral panels of the primary structure and also right and left brackets, each having a first flank connected to the right or left lateral panel of the primary structure and a second flank pressed against the right or left extension, a front engine mount having first and second links, each connected to an engine and directly to the front transverse reinforcement by a first or second reinforcement connection pin passing through the right or left extension and the second flank of the right or left bracket.

公开(公告)号：US20200307816A1

公开(公告)日：2020-10-01

申请号：US16827008

申请日：2020-03-23

Applicant: Airbus Operations SAS

Inventor： Michael BERJOT ,  Jean GELIOT

IPC: B64D27/26 ,  B64F5/10

Abstract: An aircraft rear engine attachment connecting a primary structure of a pylon and an engine of an aircraft. The rear engine attachment includes first and second rods, each of them including at least two parts, a first part including at least one support orifice, accommodating a support link bar, configured to connect the rod directly or indirectly to the primary structure, at least one second part including at least one engine orifice, accommodating an engine link bar, configured to connect the rod directly or indirectly to the engine, and also detachable link elements for connecting the first and second parts oriented parallel to the direction of the rod.