The invention relates to a ground effect aircraft capable of reducing the steering radius. A main wing of the ground effect aircraft comprises a wing surface, an aileron and a main beam, the tail end of the main beam is fixedly connected with a buoy; the buoy comprises a buoy main body, a spoiler, an aquaplane, a first driving mechanism and a second driving mechanism; one end of each of the spoiler, the water ski, the first driving mechanism and the second driving mechanism is rotationally mounted in the buoy main body; the other end of the first driving mechanism is hinged to the middle of the spoiler. The other end of the second driving mechanism is hinged to the middle of the water ski. According to the ground-effect aircraft, the aircraft body can be pressed down through the additionally arranged spoilers, so that the aircraft can press the water ski into water within a controllable range under the action of the spoilers, the resistance of the single side of the aircraft is increased, and therefore large yawing torque is obtained, and small-radius steering is achieved.

    本发明涉及一种可减小转向半径的地效飞行器,该地效飞行器的主翼包括翼面、副翼以及主梁;主梁的末端固定连接有浮筒;浮筒包括浮筒主体、扰流板、滑水板、第一驱动机构以及第二驱动机构;扰流板、滑水板、第一驱动机构以及第二驱动机构的一端均转动安装于浮筒主体内;第一驱动机构的另一端与扰流板的中部铰接;第二驱动机构的另一端与滑水板的中部铰接。该地效飞行器能够通过增设的扰流板压低机身,使飞行器在扰流板的作用下在可控的范围内将滑水板压入水中,增加飞行器单侧的阻力,从而获得较大的偏航力矩,实现小半径转向。


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    Title :

    Ground effect aircraft capable of reducing steering radius


    Additional title:

    一种可减小转向半径的地效飞行器


    Contributors:
    LI ZHUOYUAN (author)

    Publication date :

    2025-01-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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