The invention relates to the technical field of unmanned aerial vehicles, and provides a tailstock type vector propulsion variable tandem wing folding inspection unmanned aerial vehicle. The unmanned aerial vehicle comprises a fuselage, a front wing and a rear wing, wherein the front wing and the rear wing form a tandem wing layout; the front wings are mounted on the front wing folding mechanisms through tilting steering engines, and power propellers are arranged on the front wings; under the driving of the front wing folding mechanism, the front wings can be completely folded and stored in the longitudinal axis direction of the fuselage or unfolded in the transverse axis direction of the fuselage in a flight mode; the tilting steering engine can adjust the tilting angle of the front wing, the rear wing is rotationally installed on the rear wing variable swept wing mechanism, the rear wing is driven by the rear wing variable swept wing mechanism to be completely folded and stored in the longitudinal axis direction of the fuselage, and wing swept angle adjustment of 50-100 degrees is conducted in the level flight stage. Therefore, the portable storage of the unmanned aerial vehicle is realized, the crosswind influence is effectively reduced in the vertical take-off and landing stage, and the aerodynamic efficiency is optimal in the flight stage.

    本申请涉及无人机技术领域,提供了一种尾座式矢量推进可变串列翼折叠巡检无人机。该无人机中,机身以及形成串列翼布局的前机翼和后机翼;前机翼通过倾转舵机安装于前翼折叠机构上,前机翼上设置有动力螺旋桨;且在前翼折叠机构的带动下,前机翼能够完全折叠收纳于机身的纵轴方向,或者,在飞行模式下沿机身的横轴方向展开;倾转舵机能够对前机翼的倾转角度进行调节,后机翼转动安装于后翼变掠翼机构上,且在后翼变掠翼机构的带动下,后机翼完全折叠收纳于机身的纵轴方向,在平飞阶段进行50°~100°的机翼掠角调整。籍以,实现了无人机的便携收纳,在垂直起降阶段有效降低侧风影响,在飞行阶段的气动效率最优。


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    Titel :

    Tailstock type vector propulsion variable tandem wing folding inspection unmanned aerial vehicle


    Weitere Titelangaben:

    尾座式矢量推进可变串列翼折叠巡检无人机


    Beteiligte:
    WU HAIWEN (Autor:in) / GUO ZHENGLI (Autor:in) / GUO RUIRUI (Autor:in) / YANG ZHEN (Autor:in) / CAO JUN (Autor:in) / ZHANG QIANG (Autor:in) / WANG JIN (Autor:in) / MA ZHANHONG (Autor:in)

    Erscheinungsdatum :

    14.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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