The invention relates to the technical field of unmanned aerial vehicles, in particular to a hybrid power multi-shaft rotor wing unmanned aerial vehicle. The hybrid power multi-shaft rotor wing unmanned aerial vehicle comprises an unmanned aerial vehicle body. The unmanned aerial vehicle body comprises a flight control system and a multi-shaft drive system arranged inside a vehicle shell. The hybrid power multi-shaft rotor wing unmanned aerial vehicle is characterized by further comprising an oil-electricity hybrid power system, a servo module and a measurement and control module; the oil-electricity hybrid power system is composed of an oil-fired piston engine, an oil tank, an electricity generation module, a rectifier module and a lithium battery; one end of the oil-fired piston engine is connected with the oil tank through an oil pipe; the other end of the oil-fired piston engine is connected with the servo module; an output shaft of the oil-fired piston engine is connected with the electricity generation module; the electricity generation module is connected with one end of the rectifier module; the other end of the rectifier module is connected with the lithium battery in parallel and then is connected with the multi-shaft drive system; the multi-shaft drive system is composed of a plurality of single-shaft drivers. The hybrid power multi-shaft rotor wing unmanned aerial vehicle has the advantages of being long in endurance, large in load, easy to control, good in safety and the like.


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    Titel :

    Hybrid power multi-shaft rotor wing unmanned aerial vehicle


    Beteiligte:
    ZHANG YANWEI (Autor:in)

    Erscheinungsdatum :

    23.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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