The invention provides a tail single-duct propulsion unmanned aerial vehicle, relates to the technical field of unmanned aerial vehicles, and solves the technical problem of single motion mode of an unmanned aerial vehicle in the prior art. The device comprises a fuselage, a tail ducted device, wings and a driving device, the tail ducted device is connected with the tail of the fuselage, the side wall of the fuselage is detachably connected with the wings, the wings are close to the tail ducted device, the driving device is installed in the fuselage, and an output shaft of the driving device is connected with the tail ducted device; the tail duct device comprises a variable-pitch propeller mechanism, a steering mechanism and a shell, the shell is connected with the fuselage, the variable-pitch propeller mechanism is located in the shell, an output shaft of the driving device is connected with the variable-pitch propeller mechanism, and the driving device can drive the variable-pitch propeller mechanism to rotate; the steering mechanism is installed in the shell, the steering mechanism and the fuselage are located on the two sides of the variable pitch propeller mechanism respectively, and the steering mechanism can swing.
本发明提供了一种尾部单涵道推进无人飞行器,涉及无人飞行器技术领域,解决了现有技术中存在的无人飞行机运动模式单一的技术问题。该装置包括机身、尾部涵道装置、机翼和驱动装置,其中,尾部涵道装置与机身的尾部相连接,机身的侧壁与机翼可拆卸连接且机翼靠近尾部涵道装置,驱动装置安装在机身内且驱动装置的输出轴与尾部涵道装置相连接;尾部涵道装置包括变距螺旋桨机构、转向机构和壳体,壳体与机身相连接,变距螺旋桨机构位于壳体内且驱动装置的输出轴与变距螺旋桨机构相连接,驱动装置能驱动变距螺旋桨机构转动,转向机构安装在壳体内且转向机构和机身分别位于变距螺旋桨机构的两侧,转向机构能做摆动运动。
Tail single-duct propulsion unmanned aerial vehicle
尾部单涵道推进无人飞行器
2022-07-29
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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