公开(公告)号：US20240400216A1

公开(公告)日：2024-12-05

申请号：US18673984

申请日：2024-05-24

Applicant: Airbus Operations SAS

Inventor： Eric RENAUD ,  Thomas DEFORET ,  Mathieu KALETA ,  Antoine CLAVEYROLLAS ,  Mathieu MAHE ,  Ginesa TORRES LOPEZ

IPC: B64D29/06 ,  F01D25/24

Abstract: A propulsion assembly comprising a fan casing and a nacelle which comprises an air inlet which is connected to the front end of the fan casing, an intermediate portion which is positioned around the fan casing and a rear portion which cooperates with the rear end of the fan casing. The intermediate portion comprises at least one aerodynamic panel which extends from a front edge which is attached to the air inlet as far as a rear edge which is attached to the rear portion and at least one intermediate radial support comprising an internal edge which is connected to the fan casing and an external edge which is connected to the aerodynamic panel, this panel comprising a front edge which is connected to the air inlet by a first connection system. Also an aircraft with such a propulsion assembly.