The invention provides a tandem type double-duct propulsion unmanned aerial vehicle, relates to the technical field of unmanned aerial vehicles, and solves the technical problem that a vertical take-off and landing unmanned aerial vehicle in the prior art is tedious in the take-off and landing process. The device comprises a machine body, a front duct propelling structure, a rear duct propelling structure, a first driving device and a second driving device, the head of the machine body is connected with the front duct propelling structure, the tail of the machine body is connected with the rear duct propelling structure, and the first driving device is connected with the second driving device. The first driving device and the second driving device are both installed in the fuselage, an output shaft of the first driving device is connected with the front duct propelling structure, and the first driving device can control the front duct propelling structure to operate. An output shaft of the second driving device is connected with the rear duct propelling structure, and the second driving device can control the rear duct propelling structure to operate.
本发明提供了一种串列式双涵道推进无人飞行器,涉及无人飞行器技术领域,解决了现有技术中的垂直起降无人飞行机存在起降过程繁琐的技术问题。该装置包括机身、前涵道推进结构、后涵道推进结构、第一驱动装置和第二驱动装置,其中,所述机身的头部与所述前涵道推进结构相连接,所述机身的尾部与所述后涵道推进结构相连接,所述第一驱动装置和所述第二驱动装置均安装在所述机身内部,所述第一驱动装置的输出轴与所述前涵道推进结构相连接且所述第一驱动装置能控制所述前涵道推进结构运行,所述第二驱动装置的输出轴与所述后涵道推进结构相连接且所述第二驱动装置能控制所述后涵道推进结构运行。
Tandem type double-duct propulsion unmanned aerial vehicle
一种串列式双涵道推进无人飞行器
2022-07-01
Patent
Elektronische Ressource
Chinesisch
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