The invention provides an unmanned aerial vehicle structure. Opening grooves which are symmetrical in the vertical direction are formed in the two opposite sides of a fuselage of the unmanned aerial vehicle structure correspondingly, module batteries are inserted into the opening grooves correspondingly, a flying pipe box is arranged at the bottom of the fuselage, a holder is arranged at the bottom of the flying pipe box, and each module battery comprises a battery shell and a battery pack arranged in the battery shell. Pressing buckles capable of elastically stretching and retracting towards the interior of the battery shell are arranged at the tops of the two side walls, corresponding to the two opposite sides of the battery shell and the opening groove respectively, of the battery shell, each pressing buckle comprises a pressing part, a buckling part and a connecting part for connecting the pressing part and the buckling part, and buckling grooves matched with the buckling parts are formed in the tops of the two opposite sides of the opening groove respectively. The two module batteries with the same battery capacity are adopted, what is guaranteed is that the total battery capacity is not changed, the single module battery is more convenient to disassemble and assemble, and the two module batteries are symmetrically installed on the two sides of the fuselage, so that hardware such as a miniature airborne computer with the strict gravity center requirement can be placed in the center of the bottom of the fuselage; and the rationality of the overall structure layout is improved.
本发明提供了一种无人机结构,其机身的相对两侧分别设有沿竖直方向对称的开口槽,开口槽内分别插设有模块电池,机身底部设有飞管盒子,飞管盒子底部设有云台,模块电池包括电池壳体及设置在电池壳体内的电池组,电池壳体与开口槽相对两侧对应的两侧壁顶部分别设有可朝电池壳体内部弹性伸缩的按压扣,按压扣包括按压部、卡扣部及连接按压部和卡扣部的连接部,开口槽相对两侧顶部分别设有与卡扣部适配的卡扣槽,这样,采用两块同等电池容量的模块电池,保证了总电池容量不变,并且单块模块电池的拆装更便捷,两模块电池对称的方式安装在机身两侧,使得机身底部中心可以放置微型机载计算机等对重心要求较严格的硬件,提高了整体结构布局的合理性。
Unmanned aerial vehicle structure
一种无人机结构
2021-06-18
Patent
Elektronische Ressource
Chinesisch
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