The invention relates to an unmanned aerial vehicle horizontal tail structure and an unmanned aerial vehicle, the unmanned aerial vehicle horizontal tail structure comprises a horizontal tail body and a rudder lifting structure, the rudder lifting structure is connected with the horizontal tail body through a rudder supporting structure, the rudder supporting structure comprises a first connecting part and a second connecting part, and the first connecting part is fixedly connected with the horizontal tail body; the second connecting part is fixedly connected with the first connecting part, the second connecting part is provided with a connecting shaft, and the rudder lifting structure is provided with a mounting hole for accommodating the connecting shaft. In the horizontal tail structure of the unmanned aerial vehicle, the rudder lifting structure and the horizontal tail body are connected in a matched mode through the connecting shaft of the rudder supporting structure and the mounting hole, mounting and dismounting between the horizontal tail body and the rudder lifting structure are facilitated, the assembling process is simplified, and the assembling convenience of the horizontal tail structure of the unmanned aerial vehicle is improved.
本公开关于一种无人机平尾结构及无人机,无人机平尾结构包括平尾本体与舵升降结构,舵升降结构通过舵支撑结构与平尾本体连接,舵支撑结构包括第一连接部和第二连接部,第一连接部与平尾本体固定连接,第二连接部与第一连接部固定连接,第二连接部设置有连接轴,舵升降结构设置有容纳连接轴的安装孔。本公开的无人机平尾结构中,舵升降结构与平尾本体通过舵支撑结构的连接轴与安装孔配合连接,便于平尾本体与舵升降结构之间的安装与拆卸,简化了装配过程,提高了无人机平尾结构的装配便捷性。
Unmanned aerial vehicle horizontal tail structure and unmanned aerial vehicle
一种无人机平尾结构及无人机
2023-09-15
Patent
Electronic Resource
Chinese
IPC: | B64U |
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