The invention discloses a bimorphic unmanned aerial vehicle using folding wings and a coaxial double-propeller power module. The bimorphic unmanned aerial vehicle comprises a rear end cover, a front end cover, a folding mechanism and a flying mechanism which are arranged on the two sides of an aircraft shell; the folding mechanism comprises folding wings, a connecting shaft, a transmission bevel gear and an output bevel gear; the flying structure comprises a first motor shell, a connecting platform and a second motor shell. The coaxial double-propeller power module is used for providing vector power for the unmanned aerial vehicle, higher flight efficiency and load performance are achieved, power and control needed by stability of the aircraft are provided in a hovering mode, the coaxial double-propeller power module is used for pushing and controlling the aircraft, and therefore, the unmanned aerial vehicle is controlled to be in a stable state in a hovering or flying mode; the folding wings are used for providing lift force needed by the aircraft, the folding wings can be conveniently folded and stored, the aircraft body is more regular after being folded, carrying and transportation are convenient, and the voyage, hang capacity and functionality of the aircraft are greatly improved.
本发明公开了一种运用折叠机翼和共轴双桨动力模块的双形态无人机,包括飞行器壳体两侧的后端盖、前端盖、折叠机构和飞行机构;所述折叠机构包括折叠翼、连接轴、传动伞齿轮和输出伞齿轮;所述飞行结构包括第一电机壳体、连接平台和第二电机壳体。本发明运用共轴双桨动力模块提供无人机的矢量动力,拥有更高的飞行效率以及载荷性能,在悬停模式下提供飞行器稳定所需的动力和控制,利用共轴双桨动力模块完成对飞行器的推动和控制,从而将无人机控制在悬停或飞行模式下的稳定状态;利用折叠机翼提供飞机所需的升力,折叠翼可以方便的折叠收纳,折叠起来机身更为规整,便于携带与运输,极大提高飞行器的航程、滞空能力和功能性。
Bimorphic unmanned aerial vehicle using folding wings and coaxial double-propeller power module
一种运用折叠机翼和共轴双桨动力模块的双形态无人机
2021-05-28
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2021
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