A tilting wing and fixed wing mixed type unmanned aerial vehicle is characterized by comprising a rack, four fixed wings fixed in holes in the left upper direction, the left lower direction, the right upper direction and the right lower direction of the rack, four tilting parts fixed in holes in the right upper direction, the right lower direction, the right left direction and the right right direction of the rack, a machine cover covering the rack and a center control component embedded in the rack; according to the tilting wing and fixed wing mixed type unmanned aerial vehicle, through mixed work of the fixed wings and the tilting rotors, the advantages of vertical take-off and landing and hovering of a common rotor unmanned aerial vehicle are reserved, and the problems that the common rotor unmanned aerial vehicle cannot steer horizontally, the flight path is not easy to control accurately, and the common rotor unmanned aerial vehicle cannot advance at a high speed are solved. The tilting directions of the tilting rotors are controlled by the servo motors, so that the unmanned aerial vehicle can obtain high adaptability to various takeoff environments, and meanwhile, the unmanned aerial vehicle can finish accurate operation in various complicated environments due to the fact that the unmanned aerial vehicle can accurately control the flight path and the flight attitude in the air. The tilting wing and fixed wing mixed type unmanned aerial vehicle can finish accurate operations in various relatively complex environments.

    一种倾转翼、固定翼混合型无人机,其特征在于,包括:机架,固定于机架左上、左下、右上、右下四个方向孔洞中的四个固定翼,固定于机架正上、正下、正左、正右四个方向孔洞中的四个倾转部分,覆盖在机架上的机盖,镶嵌于机架内部的中心控制部件;本设计通过固定翼、倾转旋翼的混合工作,既保留了普通旋翼无人机可以实现垂直起降及空中悬停的优势,又解决了普通旋翼无人机无法水平转向、飞行轨迹不易精确控制、无法高速前行的问题。通过伺服电机对倾转旋翼倾转方向的控制,可以让本发明获得对于各种起飞环境的较高适应能力,同时由于本发明可以精确控制在空中的飞行轨迹及飞行姿态,本发明可以完成各种较复杂环境中的精确作业。


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    Titel :

    Tilting wing wing and fixed wing mixed type unmanned aerial vehicle


    Weitere Titelangaben:

    一种倾转翼、固定翼混合型无人机


    Beteiligte:
    LIU SHENGPENG (Autor:in) / WANG XUERUI (Autor:in) / CHEN JIAPING (Autor:in) / ZHANG YIFAN (Autor:in) / YANG BIYAN (Autor:in)

    Erscheinungsdatum :

    2021-07-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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