The invention relates to the technical field of aircrafts, in particular to an aerodynamic layout of a small-sized vertical takeoff and landing aircraft. The aerodynamic layout comprises a machine body, wherein two front wings, two main wings and four tail wings are sequentially arranged on the machine body in the length direction; the front wings and the main wings are mutually perpendicular; a power system is further arranged on the machine body and used for providing vertical takeoff and landing power and a horizontal flight pushing force for the small-sized vertical takeoff and landing aircraft; the vertical takeoff and landing direction of the small-sized vertical takeoff and landing aircraft is consistent with the length direction of the machine body. By the adoption of the aerodynamic layout, the horizontal flight speed of the small-sized vertical takeoff and landing aircraft is greatly improved, the advantages of high response speed and reliability are achieved during completion of various actions, and in addition, use and maintenance are facilitated.


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    Title :

    Aerodynamic layout of small-sized vertical takeoff and landing aircraft


    Contributors:
    ZHANG RUI (author)

    Publication date :

    2015-11-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge