The invention relates to the technical field of rotor unmanned aerial vehicles, in particular to an aircraft power mounting structure which comprises a power driving mechanism, the power driving mechanism comprises a mounting box, a side base plate is fixedly arranged on the outer side wall face of the mounting box, and a cavity supporting plate is fixedly arranged on the outer side of the side base plate. A first round rod is rotationally arranged on the inner wall of the top end of the mounting box, a large gear is fixedly arranged at the bottom end of the first round rod, second round rods are fixedly arranged between the inner wall of the top end and the inner wall of the bottom end of the mounting box, column casings are fixedly arranged on the outer sides of the second round rods, and silica gel arc pads are fixedly arranged on the outer sides of the column casings. According to the four-rotor unmanned aerial vehicle power assembly synchronous linkage device, a synchronous linkage structure for a four-rotor unmanned aerial vehicle power assembly is formed through the mounting box, the side base plates, the cavity supporting plates, the first round rods, the large gears, the second round rods, the column casings and the silica gel arc pads.
本发明涉及旋翼无人机技术领域,尤其为一种飞行器的动力安装结构,包括动力驱动机构,所述动力驱动机构包括安装箱,所述安装箱外侧壁面固定设置有侧垫板,所述侧垫板外侧固定设置有空腔支板,所述安装箱顶端内壁处转动设置有第一圆杆,所述第一圆杆底端固定设置有大齿轮,所述安装箱顶端内壁、底端内壁之间均固定设置有第二圆杆,所述第二圆杆外侧固定设置有柱筒,所述柱筒外侧固定设置有硅胶弧垫,所述大齿轮外侧与齿牙皮带啮合接触,本发明通过安装箱、侧垫板、空腔支板、第一圆杆、大齿轮、第二圆杆、柱筒以及硅胶弧垫形成对四旋翼无人机动力组件的同步联动结构。
Power mounting structure of aircraft
一种飞行器的动力安装结构
2023-08-29
Patent
Electronic Resource
Chinese
IPC: | B64U |