公开(公告)号：US12291340B2

公开(公告)日：2025-05-06

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: B64D27/40 ,  B64D27/30

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.