A hybrid propulsion unit for an aircraft with multi-rotor rotary wings includes an electrical generator driven by an internal combustion engine, a rectifier configured to convert an AC current sent by the electrical generator into DC current, a DC-AC converter, an electrical network connecting the rectifier to the converter and including a high-voltage DC current bus, electric motors powered by propeller converters coupled to the electric motors, electrical energy storage connected to the electrical network, the electrical storage including at least one primary storage element and at least one secondary storage element.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HYBRID PROPULSION UNIT FOR AN AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    2022-06-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64C AEROPLANES , Flugzeuge / F02B INTERNAL-COMBUSTION PISTON ENGINES , Brennkraftmaschinen mit innerer Verbrennung mit Verdrängerwirkung



    HYBRID PROPULSION UNIT FOR AN AIRCRAFT

    KLONOWSKI THOMAS / BARRACO THOMAS | Europäisches Patentamt | 2021

    Freier Zugriff

    HYBRID PROPULSION UNIT FOR AN AIRCRAFT

    KLONOWSKI THOMAS / BARRACO THOMAS | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT PROPULSION UNIT

    WAGNER JONATHAN / LANDSIEDEL BRADLEY / MILIA JOEY et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT PROPULSION UNIT

    WAGNER JONATHAN / LANDSEADEL BRADLEY / MILIA JOEY et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT PROPULSION UNIT

    SABER CHRISTELLE / MERLE SÉBASTIEN / AYAT SABRINA | Europäisches Patentamt | 2022

    Freier Zugriff