A first power source, a second power source, and a power controller are provided, where a vehicle that includes the first power source, the second power source, and the power controller is capable of flying in a transitional mode between a hovering mode and a forward flight mode. The power controller selects one or more of the first power source and the second power source to power a rotor included in the vehicle during the transitional mode.


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    Title :

    HYBRID POWER SYSTEMS FOR DIFFERENT MODES OF FLIGHT


    Contributors:

    Publication date :

    2021-04-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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 POWER SYSTEMS FOR DIFFERENT MODES OF FLIGHT

    SINHA PRANAY / VANDER LIND DAMON | European Patent Office | 2023

    Free access

    Hybrid power systems for different modes of flight

    SINHA PRANAY / VANDER LIND DAMON | European Patent Office | 2021

    Free access

    HYBRID POWER SYSTEMS FOR DIFFERENT MODES OF FLIGHT

    SINHA PRANAY / VANDER LIND DAMON | European Patent Office | 2021

    Free access

    Hybrid power systems for different modes of flight

    SINHA PRANAY / VANDER LIND DAMON | European Patent Office | 2023

    Free access

    HYBRID POWER SYSTEMS FOR DIFFERENT MODES OF FLIGHT

    SINHA PRANAY / VANDER LIND DAMON | European Patent Office | 2021

    Free access