The invention discloses a design method and system for realizing the long-endurance flight of a multi-rotor aircraft. According to the design method and system, a conventional multi-rotor aircraft (1) is powered by a solar cell, and a ground solar power panel is provided, or the flying multi-rotor aircraft (1) is powered by a hybrid power source, so that the multi-rotor aircraft (1) realizes long-endurance flight. The design method and a power supply system for realizing power supply for the ground comprise a manner for supplying power to the multi-rotor aircraft (1) flying at a fixed position, and a manner for supplying power to the multi-rotor aircraft (1) in movable flight. The design method and system, provided by the invention, also point out the design method and the system, which can realize cutting, so that users can take low expenses to realize long-endurance flight of the multi-rotor aircraft. The mature power supply design method and system, provided by the invention, realize the target of long-endurance flight, which is difficult to break through in the prior art in a short time, so that the application range of conventional multi-rotor aircrafts is enlarged.


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    Titel :

    Design method and system for realizing long-endurance flight of multi-rotor aircraft


    Beteiligte:
    TAO WENYING (Autor:in) / YANG SHAOWEN (Autor:in)

    Erscheinungsdatum :

    2015-11-04


    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



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