PROPELLER AND ELECTRIC MOTOR ASSEMBLY COMPRISING A SUITABLE PRIMARY STRUCTURE AND AIRCRAFT COMPRISING AT LEAST SUCH ASSEMBLY

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...

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Bibliographic Details
Main Authors JOLIVET, Nicolas, MERMOZ, Emmanuel, POME, Pascal, GOUPIL, Frédéric, LAPEYRE, Jean-Victor, JALBERT, Delphine, FUKASAKU, Kotaro, PENVEN, Benoît, AMARGIER, Rémi, LAFONT, Laurent, CZAPLA, Lionel, TASIC, Milan, ALVAREZ, Franck
Format Patent
LanguageEnglish
French
German
Published 18.09.2024
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Summary: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.
Bibliography:Application Number: EP20220179538