An aircraft includes a fuselage extending in a front-rear direction of the aircraft, main wings extending from sides of the fuselage, a fuel cell system located adjacent to a rear of the fuselage with respect to the main wings and configured to apply driving force to a nacelle located on each of the main wings, and a controller configured to transmit electrical energy applied from the fuel cell system to the nacelle. A center of gravity of the aircraft is located in the fuselage close to front ends of the main wings, and a flow rate of air flowing into the fuel cell system is controlled in response to an outside air condition of the aircraft.


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    Title :

    AIRCRAFT EQUIPPED WITH FUEL CELL SYSTEM AND THRUST CONTROL METHOD


    Contributors:

    Publication date :

    2024-01-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY



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