The present disclosure pertains to an unmanned aerial vehicle system. Some exemplary implementations may include: a mounting frame (110) onto which at least a payload (30) is affixed; a plurality of fuel cell stacks (50) operable in a predefined configuration, each of the plurality of stacks (50) being in a separate package; one or more tanks (60) configured to supply hydrogen to the plurality of stacks; a propulsion system (70, 80) configured to receive an output power generated from the plurality of stacks (50); and a power controller (40) configured to couple the plurality of stacks in the predefined configuration.
本公开涉及一种无人驾驶飞行器系统。一些示例性实施方式可包括:至少一个有效载荷(30)附连到其上的安装框架(110);可在预定配置中操作的多个燃料电池堆(50),该多个堆(50)中的每个都在单独封装中;被配置为向多个堆供应氢气的一个或多个储罐(60);被配置为接收从多个堆(50)生成的输出功率的推进系统(70,80);以及被配置为以预定配置耦合多个堆的电力控制器(40)。
UAV HAVING CONFIGURABLE FUEL CELL POWER SYSTEM
具有可配置燃料电池电力系统的UAV
2021-11-30
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY |