The invention particularly relates to a full-tilt large-flap rotor aircraft which comprises an aircraft body and wings and is characterized in that the wings are mounted on the aircraft head and the aircraft tail of the aircraft body; the wing comprises a fixed wing and a large flap, and the large flap is provided with a wing shaft and is rotationally connected with the fixed wing through the wing shaft; a plurality of inner rotors are fixedly connected to the large flaps, and outer rotors are arranged at the ends of the wing shafts; the tilting mechanism is mounted in the wing; the tilting mechanism is used for driving the large flap and the inner rotor to rotate; a window is arranged at the top of the machine body; in the specific working process of the embodiment, the inner rotor wing and the outer rotor wing serve as power sources of the aircraft, and take-off, landing and air flight of the aircraft are achieved; the movable wings enable the aircraft to have better aerodynamic performance in climbing, diving and various air actions; a tilting mechanism is matched, so that the large flap and the inner rotor wing are subjected to cooperative control operation control; accidents caused by faults of a single rotor wing are avoided, and the flight stability and safety of the aircraft are improved.

    本发明具体为一种全倾转大襟翼旋翼飞行器,包括机身和机翼在其特征在于,机翼安装在机身的机头和机尾;机翼包括固定机翼和大襟翼,大襟翼设有翼轴,通过翼轴与固定机翼转动连接;大襟翼上固定连接有多个内旋翼,并且翼轴的端部设置外旋翼;倾转机构安装在机翼中;所述倾转机构用于驱动大襟翼和内旋翼旋转;所述机身顶部设有视窗;在本实施例具体工作过程中,内旋翼和外旋翼作为飞行器动力来源,实现飞行器的起降以及空中飞行;并且活动式机翼使得飞行器在爬升、俯冲以及各种空中动作有更好的空气动力性能;搭配倾转机构,实现对大襟翼和内旋翼进行协同式的控制操作控制;避免单个旋翼故障引发的事故,提高飞行器的飞行稳定性以及安全性。


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    Title :

    Full-tilt large flap rotor aircraft


    Additional title:

    一种全倾转大襟翼旋翼飞行器


    Contributors:
    XIE ENLI (author)

    Publication date :

    2024-06-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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