The hydrogen fuel cell multi-rotor unmanned aerial vehicle comprises a vehicle body and a power system, the vehicle body is of an integrated center disc structure, the integrated center disc structure comprises electric piles installed on the two sides of a center disc, a gas cylinder installation position is formed in the position, between the electric piles, of the center disc, and a gas cylinder is placed on the gas cylinder installation position; a flight control assembly is further installed on the bottom face of the gas cylinder installation position. According to the unmanned aerial vehicle, a brand-new integrated center disc structure is designed, the electric piles are located on the two sides of the gas cylinder, the gas cylinder is located in the center of the vehicle body, the space structure of the unmanned aerial vehicle can be greatly reduced through the structure, the rainproof and dustproof grade of a hydrogen fuel cell is increased, and the high temperature resistance and low temperature resistance of the hydrogen fuel cell are improved; the safety of the hydrogen cylinders and the hydrogen cylinder valves is improved, the structural layout is more reasonable, meanwhile, the unmanned aerial vehicle is provided with a very good gas inlet system, a very good heat dissipation system and a better power supply management system, and the use requirements of the unmanned aerial vehicle are met.
本发明公开了一种氢燃料电池多旋翼无人机,包括机身、动力系统,机身是一个一体式的中心盘结构,一体式的中心盘结构包括安装在中心盘两侧的电堆,位于电堆之间的中心盘上形成一个气瓶安装位,气瓶放置在气瓶安装位上,气瓶安装位底面还安装有飞控组件。本发明的无人机,设计一种全新的一体式中心盘结构,使得电堆位于气瓶的两侧,气瓶位于机身主体的中心位置,这种结构可以大大缩小无人机的空间结构,增加氢燃料电池的耐防雨防尘等级,增加氢燃料电池耐高温性,低温性,增加氢气瓶及氢气瓶阀门安全性,结构布局更加的合理,同时本发明具有非常好的进气系统,散热系统,且具有更好的电源供电管理系统,满足无人机的使用需求。
Hydrogen fuel multi-rotor unmanned aerial vehicle
一种氢燃料多旋翼无人机
2022-11-01
Patent
Electronic Resource
Chinese
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