The invention provides a multi-wing aircraft which comprises an aircraft body, a plurality of pairs of wings, an engine and a tilting rotor wing part, and the wings are symmetrically distributed on the two sides of the aircraft body. The engine is arranged in the wing. The tilting rotor wing part comprises a plurality of tilting rotor wings arranged at the tail ends of the wings, and the power output end of the engine is connected with the tilting rotor wings through a transmission shaft; the tilting rotor wing comprises a tilting mechanism and a propeller arranged on the tilting mechanism, and the tilting mechanism is used for adjusting the tilting direction of the propeller. The multi-wing aircraft provided by the invention has the advantages of high maneuvering performance and high controllability, and the multi-wing aircraft can perform various flight postures or air performance.

    本申请提供的一种多翼飞行器,包括机身、多对机翼、发动机、倾转旋翼部,其中,机翼对称分布于机身的两侧。发动机设置于机翼内。倾转旋翼部包括设置于机翼末端的多个倾转旋翼,发动机的动力输出端通过传动轴与倾转旋翼相连;倾转旋翼包括倾转机构以及设置于倾转机构上的螺旋桨,倾转机构用于调节螺旋桨倾斜方向。本申请提供的多翼飞行器具有机动性能以及可操控性能高的优点,可使得多翼飞行器可进行各种飞行姿势或者空中表演。


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    Title :

    Multi-wing aircraft and control method thereof


    Additional title:

    一种多翼飞行器及其控制方法


    Contributors:
    YANG XINXIN (author)

    Publication date :

    2022-12-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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