Folding unmanned aerial vehicle

The utility model relates to an unmanned air vehicle technique field, concretely relates to folding unmanned aerial vehicle, including unmanned aerial vehicle fuselage and four rotors, four rotors setup respectively the both sides that the unmanned aerial vehicle fuselage is relative, the outside extension of both sides level that the unmanned aerial vehicle fuselage is relative is provided withfour connecting rods, connecting rod one end fixed mounting has first motor, the output shaft of first motor upwards set up and with rotor center fixed connection, unmanned aerial vehicle fuselage upper surface indent forms four holding tanks that are used for holding rotor and connecting rod, still be provided with on the unmanned aerial vehicle fuselage and be used for rotating connecting rod and rotor extremely connecting rod slewing mechanism in the holding tank. 本实用新型涉及无人机技术领域，具体涉及种折叠无人机，包括无人机机身和四个旋翼，所述四个旋翼分别设置在所述无人机机身相对的两侧，所述无人机机身相对的两侧水平向外延伸设置有四个连接杆，所述连接杆端固定安装有第电机，所述第电机的输出轴向上设置且与旋翼中心固定连接；所述无人机机身上表面内凹形成四个用于容纳旋翼以及连