Embodiments are directed towards hybrid power supply that provides electric power to a multirotor rotorcraft to extend range or flying time. In one embodiment, an internal combustion engine and fuel tank are provided that interoperate with a battery provided by a commercial multirotor rotorcraft to substantially extend flying time or flying distance.


    Access

    Download


    Export, share and cite



    Title :

    Hybrid Power Supply For Electric Multirotor Rotorcraft


    Contributors:

    Publication date :

    2017-01-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



    HYBRID MULTIROTOR VEHICLES

    GILBERT ERIC BENJAMIN | European Patent Office | 2020

    Free access

    Aerodynamic optimization hybrid multirotor

    ZHANG XIN / WANG SONG / LI XUN et al. | European Patent Office | 2015

    Free access

    Multirotor

    HE CHUNWANG | European Patent Office | 2015

    Free access

    Hybrid power rotorcraft

    LI FANGJUN | European Patent Office | 2023

    Free access