The invention discloses unmanned aerial vehicle satellite full-automatic investigation equipment which comprises a fixing plate fixed to an unmanned aerial vehicle body. A fixing clamping groove and afixing clamping plate are arranged on the fixing plate; one end of the clamping groove is closed through an end plate, a sensing hole is formed in the end plate, and a button switch of a sensing assembly is installed in the sensing hole. The fixing clamping groove and a holder clamping plate are assembled in a clamped mode, the holder clamping plate is arranged on a holder shell, the holder shellis provided with a holder clamping groove, and the holder clamping groove and the fixing clamping plate are assembled in a clamped mode. The holder shell belongs to a holder assembly. The end, away from the end plate, of the fixing clamping plate is provided with a guide groove, a locking hole and a guide slope, the locking hole and one end of a locking rod are clamped and assembled, the other end of the locking rod penetrates a holder partition plate and then is assembled with a limiting electromagnet, and the locking rod and the limiting electromagnet belong to limiting assemblies. The fixing plate is fixed to the unmanned aerial vehicle and then the holder assembly and the fixing plate are designed to be of a detachable structure, so that the holder assembly is convenient to detach.
本发明公开了一种无人机卫星全自动勘察设备,包括,固定板,固定板固定在无人机机身上,固定板上设置有固定卡合槽、固定卡合板,且卡合槽一端通过端板封闭,端板上设置有感应孔,感应孔内安装有感应组件的纽扣开关;固定卡合槽与云台卡合板卡合装配,云台卡合板设置在云台外壳上,云台外壳上设置有云台卡合槽,云台卡合槽与固定卡合板卡合装配;云台外壳属于云台组件;固定卡合板远离端板一端上设置有引导槽、锁紧孔、引导斜面,锁紧孔与锁杆一端卡合装配,锁杆另一端穿过云台隔板后与限位电磁铁装配,锁杆、限位电磁铁均属于限位组件。本发明通过在无人机上固定固定板,然后将云台组件与固定板设计为可拆卸结构,从而使得云台组件便于拆卸。
Unmanned aerial vehicle satellite full-automatic investigation equipment
无人机卫星全自动勘察设备
2020-04-17
Patent
Electronic Resource
Chinese
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