The invention discloses an unmanned aerial vehicle with a multi-driving system, and the unmanned aerial vehicle comprises a framework; two front arms are symmetrically arranged on the two sides of the front portion of the framework, two rear arms are symmetrically arranged on the two sides of the rear portion of the framework in a front-back mode, propellers are arranged at the tail ends of the front arms and the tail ends of the rear arms respectively, the framework is connected with the front arms through front arm rotating wheels, and the front arm rotating wheel enables the front arm to rotate along a rotating shaft perpendicular to the side surface of the framework; the framework is connected with the rear arm through a rear arm hinge, and the rear arm hinge enables the rear arm to rotate along a rotating shaft parallel to the side face of the framework. Two airbag shells are symmetrically fixed to the two sides of the bottom of the framework, each airbag shell is a semi-cylindrical cover parallel to the side face of the framework, an airbag is arranged in each airbag shell, and each airbag is provided with an electromagnetic exhaust valve. Compared with the prior art, the unmanned aerial vehicle can float on the water surface to run and rotate, so that the unmanned aerial vehicle can execute tasks on the water surface and in the air, and when the air bag is not inflated, movement of the sliding block assembly in the direction of the front arm is locked.
本发明公开了:一种具有多驱动系统的无人机,包括构架,其中,所述构架的前部两侧对称地设有两根前臂,所述构架的后部两侧前后对称的设有两根后臂,且所述前臂与后臂末端各设有螺旋桨,所述构架与前臂通过前臂转轮连接,所述前臂转轮使得前臂能够沿与构架侧面垂直的转轴转动;所述构架与后臂通过后臂铰链连接,所述后臂铰链使得后臂能够沿与构架侧面平行的转轴转动;所述构架底部的两侧对称地固定有两个气囊壳体,所述气囊壳体为与构架侧面平行的半圆柱型罩体,其内设有气囊,所述气囊设有电磁排气阀;与现有技术相比,本发明能够在漂浮在水面上行驶和旋转,使其能够执行水面和空中的任务,当气囊未充气时,滑块组件向前臂方向的移动被锁止。
Unmanned aerial vehicle with multiple driving systems
一种具有多驱动系统的无人机
2021-07-09
Patent
Electronic Resource
Chinese
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