The invention discloses a cross-medium aircraft capable of vertically taking off and landing, and relates to the technical field of aircraft design, the cross-medium aircraft comprises an aircraft body, the middle of the aircraft body is provided with at least two ducted cylinders, the ducted cylinders penetrate through the aircraft body in the vertical direction, each ducted cylinder is internally provided with a group of rotor wings, and each group of rotor wings are driven by different first driving units; a plurality of propellers are installed at the tail of the fuselage, the propellers are driven by different second driving units respectively, and a tilting assembly is further arranged in the fuselage, connected with the rotors and capable of driving the rotors to tilt synchronously. The unmanned aerial vehicle is good in aerodynamic performance, and the posture and direction can be rapidly adjusted during air flight and underwater sneaking.

    本发明公开了一种可垂直起降的跨介质飞行器,涉及飞行器设计技术领域,包括机身,机身的中部有至少两个涵道筒,涵道筒在竖直方向上贯通机身,各涵道筒内分别安装有一组旋翼,各组旋翼分别通过不同的第一驱动单元驱动,机身的尾部安装有若干个螺旋桨,各螺旋桨分别通过不同的第二驱动单元驱动,机身内还设有倾转组件,倾转组件连接各旋翼,并能够带动各旋翼同步倾转。本发明气动性能好,且能够实现空中飞行、水下潜行时快速调整姿态和方向。


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    Title :

    Cross-medium aircraft capable of vertically taking off and landing


    Additional title:

    一种可垂直起降的跨介质飞行器


    Contributors:
    ZHAO QIJUN (author) / LIANG CHENGLIANG (author) / FEI ZHONGYANG (author) / CHEN XI (author) / ZHAO GUOQING (author) / CHEN ZHE (author) / YANG TAO (author) / MA LI (author)

    Publication date :

    2024-11-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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