The invention discloses a loading unmanned aerial vehicle take-off and landing frame which comprises a buffer frame, a rotating end is welded to the lower end of the buffer frame, a rotating groove is formed in the outer side of the rotating end through a rotating shaft, a lower damping shaft is installed on the outer side of the rotating groove through a bolt, and the lower damping shaft is axially connected with the rotating shaft between the rotating end and the rotating groove. A supporting block is welded to the lower portion of the rotating groove, a grounding support is installed at one end of the supporting block through a bolt, an installation pipe is installed at one end of the grounding support through a bolt, compressed air is embedded in one side of the installation pipe, and the installation pipe and the compressed air are fixed and sealed through a fixing hoop. By arranging the lower damping shaft, the upper damping shaft, the grounding support, the mounting pipe, the buffer feet, the mounting support and the limiting traction part, the problems that an existing carrier unmanned aerial vehicle take-off and landing frame is still poor in buffer effect, cannot provide lift force for an unmanned aerial vehicle and cannot provide buffer force for landing of the unmanned aerial vehicle are solved.
本发明公开了一种载物无人机起降架,包括缓冲架,在缓冲架的下端焊接有旋转端头,在旋转端头的外侧通过转轴安装有旋转槽,在旋转槽的外侧通过螺栓安装有下方阻尼轴,且下方阻尼轴与旋转端头和旋转槽之间的转轴向连接,在旋转槽的下方焊接有支撑块,在支撑块的一端通过螺栓安装有接地支架,在接地支架的一端通过螺栓安装有安装管,在安装管的一侧的内部镶嵌有压缩空气,且安装管和压缩空气之间通过固定箍进行固定以及密封。本发明通过设置下方阻尼轴,上方阻尼轴,接地支架,安装管,缓冲脚,安装支架和限定牵引,解决现有载物无人机起降架依然存在着的缓冲效果差,不能为无人机提供升力,不能为无人机降落提供缓冲力的问题。
Loading unmanned aerial vehicle take-off and landing frame
一种载物无人机起降架
2021-05-18
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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