The invention provides a peak group combat unmanned aerial vehicle. The peak group combat unmanned aerial vehicle comprises a fuselage, a nose, wings, a vertical fin, an electric control assembly, safety protection equipment and a torsional spring, the nose, the wings, the vertical fin, the electric control assembly, the safety protection equipment and the torsion spring are all arranged on the fuselage; the wings comprise a left front wing, a right front wing, a left rear wing and a right rear wing; the left front wing and the right front wing are connected together through a torsion spring; the left rear wing and the right rear wing are connected together through a torsion spring; the vertical fin is connected with the fuselage through a torsion spring; the torsion springs are used for enabling the left front wing, the right front wing, the left rear wing, the right rear wing, the vertical fin and the fuselage to bear torsion in a folded state; the right front wing is mounted on the left front wing; and the left rear wing is mounted on the right rear wing. The unmanned aerial vehicle is designed into the folding wings, the wings can be folded to be attached to the vehicle body during transportation, the vertical fin, the propeller and the like need to be folded, and the occupied space and the size of the unmanned aerial vehicle are saved to the maximum extent.

    本发明提供了一种峰群作战无人机,包括:机身、机头、机翼、垂尾、电控组件、安全保护设备和扭簧;机头、机翼、垂尾、电控组件、安全保护设备和扭簧均设置在机身上;机翼包括:左前机翼、右前机翼、左后机翼和右后机翼;左前机翼和右前机翼通过扭簧连接在一起;左后机翼和右后机翼通过扭簧连接在一起;垂尾通过扭簧与机身连接;扭簧用于使左前机翼和右前机翼、左后机翼和右后机翼以及垂尾和机身在折叠状态上承受扭力;右前机翼安装在左前机翼的上面;左后机翼安装在右后机翼的上面。本发明的无人机设计成折叠式机翼,运输的时候机翼可以折叠起来贴合机身,垂尾,螺旋桨等都要折叠,做到最大限度的节省占用空间和自身体积。


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    Title :

    Peak group combat unmanned aerial vehicle


    Additional title:

    一种峰群作战无人机


    Contributors:
    LU SHIXIA (author)

    Publication date :

    2024-01-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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