A hybrid electric system for a rotorcraft can include a first thermal engine, a second thermal engine, and an electrical machine. The first thermal engine can be sized to produce a maximum first thermal engine power that is below a one-or-more-engine-inoperative (OEI) requirement power and the second thermal engine can be sized to produce a maximum second thermal engine power that is below the OEI requirement power. The electrical machine can be sized to provide at least a remaining power needed to reach the OEI requirement power in an OEI state.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    HYBRID ELECTRIC SYSTEMS FOR ROTORCRAFT


    Beteiligte:

    Erscheinungsdatum :

    2022-09-22


    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



    HYBRID ELECTRIC SYSTEMS FOR ROTORCRAFT

    MARK MICHAEL R / GUERCHKOVITCH LEONID | Europäisches Patentamt | 2022

    Freier Zugriff

    HYBRID ELECTRIC SYSTEMS FOR ROTORCRAFT

    MARK MICHAEL R / GUERCHKOVITCH LEONID | Europäisches Patentamt | 2022

    Freier Zugriff

    Hybrid electric system for rotorcraft

    MACK MATTHEW R / GRCKOVICH LEONID | Europäisches Patentamt | 2022

    Freier Zugriff

    Man-electric hybrid double-layer rotorcraft

    WANG ZHICHENG | Europäisches Patentamt | 2021

    Freier Zugriff

    HYBRID ROTORCRAFT

    HIRAIWA KAZUYOSHI | Europäisches Patentamt | 2023

    Freier Zugriff