An aircraft propulsion unit with an engine mount connecting a rigid casing, supporting a propeller, and a structure. First and second transverse link rods connect the casing and the structure with first and second joints each having an axis of pivoting substantially parallel to an axis of rotation of the propeller. First and second thrust rods connect the casing and the structure by first and second thrust rod connections. The first and second thrust rod connections separated from one another in the longitudinal direction. A longitudinal end stop is configured to limit the movement of the casing with respect to the structure in at least the longitudinal direction. An aircraft with at least one such propulsion unit.


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    Titel :

    Compact electric propulsion unit comprising a statically determinate engine mount, and aircraft comprising at least one such electric propulsion unit


    Beteiligte:
    AMARGIER RÉMI (Autor:in) / FUKASAKU KOTARO (Autor:in)

    Erscheinungsdatum :

    06.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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




    ELECTRIC PROPULSION UNIT COMPRISING AT LEAST TWO INDEPENDENT SUPPORTS, AIRCRAFT COMPRISING AT LEAST ONE SUCH ELECTRIC PROPULSION UNIT

    FUKASAKU KOTARO / AMARGIER RÉMI / CZAPLA LIONEL et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Propulsion unit for aircraft and aircraft comprising at least one such propulsion unit

    CZAPRA LIONEL / PISAVIN ALEXEY | Europäisches Patentamt | 2024

    Freier Zugriff