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

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...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: 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
Sprache:eng ; fre ; ger
Schlagworte:
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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Beschreibung
Zusammenfassung: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.