公开(公告)号：US12214890B2

公开(公告)日：2025-02-04

申请号：US18355779

申请日：2023-07-20

Applicant: Airbus Operations SAS

Inventor： Mathieu Mahe ,  Christophe Labarthe ,  Frederic Journade ,  Frédéric Vinches ,  Franck Alvarez ,  Lionel Czapla ,  Emmanuel Vardelle ,  Rémi Amargier ,  Kotaro Fukasaku

IPC: B64D27/40 ,  B64D27/24 ,  B64D27/30 ,  B64D27/355 ,  B64D41/00 ,  H01M8/2465

Abstract: A propulsion unit, for an aircraft, comprising a hollow chassis with an opening at the bottom, a propulsion system comprising an electric motor with a propeller, a fuel cell, a tank and a cooling system, and one platform fastened to the chassis through said opening using fasteners and in which at least one element of the propulsion system is fastened to the platform. An aircraft with such a propulsion unit.