The invention provides a composite lift force type unmanned aerial vehicle realizing vertical take-off and landing and aims to provide a composite lift force type unmanned aerial vehicle which is simple in structure and easy to manufacture, can hover and vertically take off and land, can fly flatly at a high speed and can fly for long endurance. The composite lift force type unmanned aerial vehicle comprises a body, wings, auxiliary bodies, vertical tails, a horizontal tail, an undercarriage, a main propeller power system, auxiliary propeller motor systems, a comprehensive energy device, a navigation device and a comprehensive control device. The composite lift force type unmanned aerial vehicle has the design characteristics as follows: due to structure combination of a fixed wing and multiple rotor wings, the composite lift force type unmanned aerial vehicle simultaneously has advantages of high speed, high efficiency and long-endurance flight of a fixed-wing unmanned aerial vehicle and advantages of vertical take-off and landing and hovering flight of a multi-rotor-wing unmanned aerial vehicle, has long endurance time and high flight efficiency, is simple in structure and can vertically take off and land and hover by means of a composite lift force system, the unmanned aerial vehicle can take off and land without field limitation, and the efficient and long-endurance flight requirements are met.


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    Title :

    Composite lift force type unmanned aerial vehicle realizing vertical take-off and landing


    Contributors:
    LIAN BIN (author) / YANG JINMING (author)

    Publication date :

    2015-12-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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