公开(公告)号：US11565822B2

公开(公告)日：2023-01-31

申请号：US16708760

申请日：2019-12-10

Applicant: Airbus Operations SAS

Inventor： Philippe Auge ,  Benoit Orteu ,  Julien Bernat ,  Jean Geliot ,  Delphine Jalbert ,  Frédéric Ridray ,  Laurent Lafont ,  Pascal Gardes

IPC: B64D27/26 ,  B64D27/18 ,  B64D29/06 ,  F02C7/20 ,  F02K3/06

Abstract: A propulsion assembly having a pylon, a turbomachine comprising an engine and a fan that is enclosed by a fan casing, a nacelle surrounding the engine and the fan casing and having a load support disposed in the top part of the nacelle, a front engine attachment between the pylon and a front part of the engine, a rear engine attachment between the pylon and a rear part of the engine, a front fan attachment between the fan casing and the load support, and a rear pylon attachment between the pylon and the load support. Such a propulsion assembly allows a reduction in bulk since the load of the turbojet engine is distributed between the load support and the pylon, and the pylon is attached to the engine.