An unmanned aerial vehicle with a parachute comprises an unmanned aerial vehicle body and a parachute module. The parachute module comprises a base, a cover body, an inflatable material, a parachute and an inflation device. The base is arranged on the unmanned aerial vehicle body. The cover body covers the base, and a containing space is formed between the cover body and the base. The inflatable material is arranged on the base and folded in the containing space. The parachute is connected to the inflatable material and the cover body and is folded in the containing space. The inflation device is disposed on the base and connected to the inflatable material. When the inflatable material is inflated by the inflation device, the inflatable material expands and impacts the cover body, so that the cover body is separated from the unmanned aerial vehicle body, the distance between the parachute and the unmanned aerial vehicle body is increased, and the parachute is driven to be unfolded. In addition, the control mode of the unmanned aerial vehicle is also mentioned.
一种具有降落伞的无人机,包括无人机主体及降落伞模块。降落伞模块包括基座、罩体、可充气材、降落伞及充气装置。基座配置于无人机主体上。罩体覆盖于基座上而在罩体与基座之间形成容纳空间。可充气材配置于基座上而收合于容纳空间内。降落伞连接于可充气材与罩体且收合于容纳空间内。充气装置配置于基座上且连接于可充气材。当充气装置对可充气材进行充气时,可充气材膨胀并撞击罩体而使罩体分离于无人机主体,以增加降落伞与无人机主体之间的距离并带动降落伞展开。此外,此无人机的控制方式亦被提及。
Unmanned aerial vehicle with parachute and control method of unmanned aerial vehicle
具有降落伞的无人机及其控制方法
2022-01-07
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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