公开(公告)号：US20240327008A1

公开(公告)日：2024-10-03

申请号：US18618130

申请日：2024-03-27

Applicant: Airbus Operations SAS

Inventor： Olivier PAUTIS ,  Laurent AGOSTINI ,  Jérôme COLMAGRO

IPC: B64D27/40 ,  B64D27/18

CPC classification number: B64D27/402 ,  B64D27/18

Abstract: The invention relates to a propulsion assembly having a jet engine with an intermediate casing with a rear face and a core casing to the rear of the intermediate casing, and an attachment pylon with a frontal wall and two lateral walls, a front engine attachment having a front fitting fastened in an articulated manner via two lateral fastening points to the rear face and in a rigid manner via an upper fastening zone to the frontal wall, and an intermediate engine attachment comprising a front link rod and a rear link rod on each side. Each of the link rods is mounted in an articulated manner between the front fitting and the lateral wall. With such an arrangement, the bulk of the engine attachments is reduced in the bypass flow.