Disclosed is a hybrid multirotor propulsion system (100) for an aircraft, comprising: a plurality of propulsion units (PU), each propulsion unit (PU) comprising a propeller (Pr), an electromotor (EU) and a peripheral differential gearbox (PDGU); a plurality of driving elements (PDS), each of which being coupled to a respective one of said plurality of propulsion units (PU); a mechanical power source (MPS); a main distributor gearbox (MDG); at least one electric machine (EM); and a power management unit (PMU); wherein said power management unit (PMU). The PMU is configured to cause distribution of mechanical and electrical power within the multirotor propulsion system.


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    Titel :

    HYBRID MULTIROTOR PROPULSION SYSTEM FOR AN AIRCRAFT


    Weitere Titelangaben:

    HYBRIDES MULTIROTOR-ANTRIEBSSYSTEM FÜR EIN FLUGZEUG
    SYSTÈME DE PROPULSION MULTIROTOR HYBRIDE-POUR AÉRONEF


    Beteiligte:
    KLEIN VILKO (Autor:in) / JURANIC JASMIN (Autor:in) / KOVAC LEVANTIN JOSIP (Autor:in) / NIKOLIC IVAN (Autor:in)

    Erscheinungsdatum :

    07.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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