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.
ENSEMBLE PROPULSEUR À HÉLICE ET MOTEUR ÉLECTRIQUE COMPRENANT UNE STRUCTURE PRIMAIRE ADAPTÉE ET AÉRONEF COMPORTANT AU MOINS UN TEL ENSEMBLE PROPULSEUR
PROPELLER AND ELECTRIC MOTOR ASSEMBLY COMPRISING A SUITABLE PRIMARY STRUCTURE AND AIRCRAFT COMPRISING AT LEAST SUCH ASSEMBLY
PROPELLER- UND ELEKTROMOTORBAUGRUPPE, DIE EINE ANGEPASSTE PRIMÄRSTRUKTUR UMFASST, UND FLUGZEUG, DAS MINDESTENS EINE SOLCHE BAUGRUPPE UMFASST
2024-09-18
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2022
|ENSEMBLE PROPULSEUR POUR AERONEF ET AERONEF COMPORTANT AU MOINS UN TEL ENSEMBLE PROPULSEUR
European Patent Office | 2015
|European Patent Office | 2021
|European Patent Office | 2021
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