The invention provides a power driver of an unmanned aerial vehicle. The power driver comprises a main body, a fluid actuating system and a controller; the fluid actuating system comprises a driving area, a confluence chamber, a plurality of valves and a fluid output area; the driving area is formed by connecting a plurality of flow guide units in series, in parallel or in series-parallel combinedmanner; each flow guide unit can generate pressure difference in the flow guide unit after being enabled, so that fluid is sucked in, shunted through flow guide channels and accumulated and stored through the confluence chamber; the transmission amount of the fluid is increased when output is needed; and the output transmission amount of the shunted fluid of the flow guide channels can be controlled by the controller through the multiple valves and then gathered to the fluid output area, so that a needed transmission amount can be outputted.
本案提供一种无人飞行器的动力驱动器,包括主体、流体作动系统以及控制器,流体作动系统更包含驱动区、汇流腔室、多个阀及流体输出区。驱动区由多个导流单元串联、并联或串并联的排列方式所构成,每一导流单元可在致能后于自身内部产生压力差,借以吸入流体并经导流通道分流,以及透过汇流腔室累积储存流体,在需求输出时供输加大流体传输量,且导流通道的分流能透过多个阀以控制器来控制其分流的流体输出传输量,再汇集到流体输出区,以输出需求传输量。
Power driver of unmanned aerial vehicle
无人飞行器的动力驱动器
2020-06-23
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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