公开(公告)号：US20220411084A1

公开(公告)日：2022-12-29

申请号：US17849895

申请日：2022-06-27

Applicant: Airbus Operations SAS ,  Airbus SAS

Inventor： Pascal POME ,  Nicolas JOLIVET ,  Rémi AMARGIER ,  Lionel CZAPLA ,  Franck ALVAREZ ,  Kotaro FUKASAKU ,  Benoît PENVEN ,  Delphine JALBERT ,  Laurent LAFONT ,  Milan TASIC ,  Frédéric GOUPIL ,  Jean-Victor LAPEYRE ,  Emmanuel MERMOZ

IPC: B64D27/24 ,  B64D27/26

Abstract: A propulsion unit, and an aircraft, with a propeller and electric motor, including at least one intermediate element interposed between the electric motor and the propeller and configured to transmit at least thrust loads generated by the propeller, a primary structure supporting the propulsion unit, at least one interface having: a first load path, configured to transmit loads perpendicular to the axis of rotation of the propeller, linking the at least one intermediate element to a support linked rigidly to or incorporated in the primary structure, a second load path, configured to transmit loads that are parallel to the axis of rotation of the propeller, linking the at least one intermediate element to a support linked rigidly to or incorporated in the primary structure.