The invention relates to an unmanned aerial vehicle, in particular to a remote sensing unmanned aerial vehicle structure which comprises a flight support, two swing mechanisms, two flight arms and two flight mechanisms, the two swing mechanisms are connected to the flight support, the two flight arms are connected to the two swing mechanisms correspondingly, the two flight mechanisms are connected to the two swing mechanisms and the two flight arms correspondingly, the device can be supported on the ground through a supporting mechanism, the swing mechanisms drive the flight arms to swing at multiple positions, and the flight arms drive the flight mechanisms to be folded and unfolded. The flight mechanisms are driven by the swing mechanisms and the flight arms to move in multiple directions, the position of each flight mechanism can be greatly changed, and meanwhile, an impact mechanism starts an auxiliary flight effect in the take-off and flight processes of the device, so that the device can perform catapult-assisted take-off and can suddenly accelerate in the flight process.
本发明涉及无人机,更具体的说是一种遥感无人机结构,包括飞行支架、摆动机构、飞行臂和飞行机构,所述摆动机构设置有两个,飞行臂设置有两个,飞行机构设置有两个,两个摆动机构均连接在飞行支架上,两个飞行臂分别连接在两个摆动机构上,两个飞行机构分别连接在两个摆动机构和两个飞行臂上,可以通过支撑机构对装置进行地面上的支撑,摆动机构驱动飞行臂进行多位置的摆动,飞行臂带动飞行机构进行收展,进而在摆动机构和飞行臂的带动下飞行机构进行多方位运动,可以大幅度的改变飞行机构的位置,同时冲击机构在装置的起飞和飞行过程中,启动辅助飞行的作用,使得装置可以进行弹射起飞,并且可以在飞行中突然加速。
Remote sensing unmanned aerial vehicle structure
一种遥感无人机结构
2021-04-13
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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