The invention discloses a suspension type unmanned aerial vehicle carrying device which comprises an unmanned aerial vehicle body, a suspension body, a carrying plate and a fixing rod. The top of the unmanned aerial vehicle body is partially recessed inwards to form a storage groove used for storing the suspension body, and the suspension body capable of floating above the unmanned aerial vehicle body after being filled with quantitative helium is fixedly arranged in the storage groove. At least two fixing rods are vertically and detachably assembled on the two sides of a loading plate used for loading loads at intervals respectively, through holes in one-to-one correspondence with all the fixing rods are vertically formed in each wing of the unmanned aerial vehicle body in a penetrating mode, and the top of each fixing rod penetrating out of the corresponding through hole is fixed to a suspension body. According to the suspension type unmanned aerial vehicle carrying device, the problems that in the prior art, a carrying device is directly fixed to wings of an unmanned aerial vehicle, loads directly act on the wings in the using process, and the wings are prone to being broken due to the fact that the unmanned aerial vehicle is small in size, the wings of the unmanned aerial vehicle are small, and the strength loads of the wings can be limited are solved.
本发明公开了一种悬吊式无人机载物装置,包括:无人机本体、悬浮体、载物板和固定杆;无人机本体的顶部部分向内凹槽形成用于收纳悬浮体的收纳凹槽,且该收纳凹槽内固定设置有向其内部充入定量的氦气后能够漂浮在无人机本体上方的悬浮体,用于装载负载的载物板的两侧分别间隔且竖直可拆卸式地装配有至少两根固定杆,无人机本体的每个机翼上分别竖直贯穿开设有与所有固定杆一一对应的通孔,从该通孔穿出的每根固定杆的顶部均固定在悬浮体上,该悬吊式无人机载物装置克服现有技术中将载物装置直接固定在无人机机翼上,在使用过程中,直接将负载作用在机翼上,而由于无人机体积小,其机翼也小,机翼强度负载能够有限,会容易导致机翼被折断的问题。
Suspension type unmanned aerial vehicle carrying device
一种悬吊式无人机载物装置
2024-02-06
Patent
Electronic Resource
Chinese