The invention relates to a fixed-wing unmanned aerial vehicle. The fixed-wing unmanned aerial vehicle comprises a fuselage, a first wing, a second wing and a power mechanism, the first wing and the second wing are arranged on the two sides of the fuselage correspondingly, the first wing comprises a first connecting part and a first folding part, the first connecting part is connected with one side of the fuselage, and the first folding part is connected with the first connecting part in a foldable mode; the second wing comprises a second connecting part and a second folding part, the second connecting part is connected with the other side of the fuselage, and the second folding part is connected with the second connecting part in a foldable mode; the power mechanisms are arranged on the two sides of the fuselage and detachably connected with the first wing and the second wing. The fixed-wing unmanned aerial vehicle has the advantages of being convenient to store and carry and high in stability.
本申请涉及一种固定翼无人机。本申请所述的固定翼无人机,包括机身、第一机翼、第二机翼和动力机构,第一机翼和第二机翼分别设置于机身的两侧,第一机翼包括第一连接部和第一折叠部,第一连接部与机身的一侧连接,第一折叠部可折叠地连接第一连接部;第二机翼包括第二连接部和第二折叠部,第二连接部与机身的另一侧连接,第二折叠部可折叠地连接第二连接部;动力机构设置于机身两侧,且动力机构与第一机翼和第二机翼可拆卸地连接。本申请所述的固定翼无人机具有方便收纳和携带、稳定性高的优点。
Fixed-wing unmanned aerial vehicle
固定翼无人机
16.01.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64U |