An aircraft can include an electrical energy system including at least one battery having a plurality of cells, at least one fuel tank, one or more electrical motors powered by the electrical energy system and configured to drive one or more rotors for providing vertical thrust, and at least one fluid fueled engine operatively connected to the at least one fuel tank to drive a thruster for forward propulsive force.


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    Title :

    HYBRID AIRCRAFT


    Contributors:
    ELLER EREZ (author)

    Publication date :

    2019-03-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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