The invention relates to a symmetric hexrcopter, which belongs to the technical field of aircrafts and comprises an airframe, a left composite wing, a right composite wing, a support, front rotor wings, rear rotor wings and an undercarriage. A control system and an airborne device are arranged in the airframe. The left composite wing and the right composite wing have the same structure and are symmetrically arranged on the left side and the right side of the airframe. The front rotor wings and the rear rotor wings have the same structure and are respectively arranged on the front end and the rear end of the airframe through the support. The undercarriage adopts a jumper and wheel type composite structure. The left composite wing and the right composite wing have the same structure and are symmetrically arranged on the left side and the right side of the airframe. The left composite wing and the right composite wing are respectively provided with two rotor wings internally, and each rotor wing is driven by an engine. Vanes of the left composite wing comprises front vanes and rear vanes capable of deflecting around a wing axis. The symmetric hexrcopter can be lifted vertically by only a small take-off and land zone. The symmetric hexrcopter generates larger lifting force, and is safe, stable and flexible.


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    Title :

    Symmetric hexrcopter


    Contributors:

    Publication date :

    2016-01-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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