The invention provides a tilt rotor wing unmanned aerial vehicle. The tilt rotor wing unmanned aerial vehicle comprises a fuselage 1, wings 2 symmetrically arranged on the two sides of the fuselage 1, a V-shaped empennage 3 arranged on the fuselage 1, an even number of wing propellers 4, a tail propeller 5 and an insertion lug structure 6. Wherein the wing propellers 4 are fixed on the wings 2 on the two sides and are symmetrically distributed, the pulling force direction of the wing propellers 4 is forward in the chord length direction of the wings 2, and the wing propellers 4 are driven by tilting of the wings 2 to tilt; the tail propeller 5 is fixed at the tail end of the fuselage 1 along the central axis of the fuselage 1 through an insertion lug structure 6, and tilts by taking the direction parallel to the wingspan direction as an axis; when the unmanned aerial vehicle takes off and lands vertically and hovers at fixed points, the wing propellers 4 tilt upwards until the rotating surfaces of the wing propellers 4 are parallel to the ground, and the tail propellers 5 tilt downwards until the rotating surfaces of the tail propellers 5 are parallel to the ground.

    本发明提供了一种倾转翼无人机,包括:机身1、对称设置在机身1两侧的机翼2、设置在机身1的V型尾翼3、偶数个机翼螺旋桨4、1个尾部螺旋桨5和插耳结构6;其中:机翼螺旋桨4固定在两侧的机翼2上,对称分布,机翼螺旋桨4的拉力方向沿机翼2的弦长方向向前,并在机翼2倾转的带动下倾转;尾部螺旋桨5沿机身1的中轴线通过插耳结构6固定于机身1的尾端,以平行于翼展方向为轴倾转;当无人机垂直起降和定点悬停时,机翼螺旋桨4向上倾转至其旋转面与地面平行,尾部螺旋桨5向下倾转至其旋转面与地面平行。


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    Titel :

    Tilting rotor wing unmanned aerial vehicle


    Weitere Titelangaben:

    一种倾转翼无人机


    Beteiligte:
    BAI QIANGQIANG (Autor:in) / ZHANG SHUO (Autor:in) / LIANG YANG (Autor:in) / ZHENG YANWU (Autor:in)

    Erscheinungsdatum :

    2022-09-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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