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.


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    Titel :

    ENSEMBLE PROPULSEUR À HÉLICE ET MOTEUR ÉLECTRIQUE COMPRENANT UNE STRUCTURE PRIMAIRE ADAPTÉE ET AÉRONEF COMPORTANT AU MOINS UN TEL ENSEMBLE PROPULSEUR


    Weitere Titelangaben:

    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


    Beteiligte:
    POME PASCAL (Autor:in) / JOLIVET NICOLAS (Autor:in) / AMARGIER RÉMI (Autor:in) / CZAPLA LIONEL (Autor:in) / ALVAREZ FRANCK (Autor:in) / FUKASAKU KOTARO (Autor:in) / PENVEN BENOÎT (Autor:in) / JALBERT DELPHINE (Autor:in) / LAFONT LAURENT (Autor:in) / TASIC MILAN (Autor:in)

    Erscheinungsdatum :

    18.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT