The invention discloses a coaxial composite wing electric vertical take-off and landing aircraft, which belongs to the field of aviation and comprises an aircraft body, wings, a vertical tail and a horizontal tail, ailerons are arranged on the wings, a rudder is arranged on the vertical tail, and an elevator is arranged on the horizontal tail; lifting assemblies are mounted on the wings, and propelling assemblies are mounted on the rear sides of the horizontal empennages; the lifting assembly comprises a lifting support arm fixedly connected with the wing and two lift motors fixedly mounted on the upper side and the lower side of the lifting support arm respectively, lift propellers are mounted on the lift motors, and the two lift motors are coaxially arranged; the propelling assembly comprises a propelling supporting arm fixedly connected with the horizontal tail wing and a propelling motor fixedly installed on the propelling supporting arm, and a propelling propeller is installed on the propelling motor. Compared with the prior art, the aircraft body can be prevented from being affected by lateral force, the torque of the propellers can be balanced, and a flight control system does not need to carry out additional torque balancing operation.

    本发明公开了一种共轴复合翼电动垂直起降飞机,属于航空领域,包括机身、机翼、垂直尾翼和水平尾翼,机翼上设有副翼,垂直尾翼上设有方向舵,水平尾翼上设有升降舵;机翼上安装有升降组件,水平尾翼的后侧安装有推进组件;升降组件包括与机翼固定连接的升降支臂以及两个分别固定安装在升降支臂的上下两侧的升力电机,升力电机上均安装有升力螺旋桨,两个升力电机共轴布置;推进组件包括与水平尾翼固定连接的推进支臂以及固定安装在推进支臂上的推进电机,推进电机上安装有推进螺旋桨。相比于传统技术,本发明不但能够避免机身受到侧向力的影响,而且还能够平衡推进桨的扭矩,使飞行控制系统无需进行额外的扭矩配平操作。


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    Title :

    Coaxial composite wing electric vertical take-off and landing aircraft


    Additional title:

    一种共轴复合翼电动垂直起降飞机


    Contributors:

    Publication date :

    2024-04-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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