The invention provides a vertical take-off and landing unmanned aerial vehicle and a full-wing tilting structure thereof.The full-wing tilting structure is applied to a four-rotor tilting unmanned aerial vehicle and comprises a fuselage sliding rail, a sliding block, a connecting rod and a movable wing, the fuselage sliding rail is of a rail structure and is arranged on the upper side of a fuselage from the root of an empennage of the unmanned aerial vehicle to the middle of the unmanned aerial vehicle, and the sliding block is arranged on the fuselage sliding rail; the sliding block is arranged on the machine body sliding rail and slides on the machine body sliding rail; wings on the two sides of the unmanned aerial vehicle are each provided with a connecting rod, one end of each connecting rod is fixedly connected with the position where an inner side motor on a movable wing of the unmanned aerial vehicle is located, and the other end of each connecting rod is connected with a sliding block; movable wings are arranged on the side surfaces of the front end of the unmanned plane body; the wing fixed end is a trapezoidal mechanism and is fixedly arranged on the side face of the front end of the unmanned aerial vehicle body, and the wing movable end and the wing fixed end are connected through a rotating hinge; and the sliding block on the fuselage sliding rail drives the movable wing connected with the connecting rod to rotate around the hinge at the wing root.
本申请提供一种可垂直起降无人机及其全机翼倾转结构,所述全机翼倾转结构应用于四旋翼倾转无人机,包括机身滑轨、滑块、连杆和活动机翼,其中:机身滑轨为轨道结构,设置在无人机尾翼根部至无人机中部的机身上侧,滑块设置在机身滑轨上,在机身滑轨上滑动;无人机两侧机翼分别设置一个连杆,所述连杆的一端与无人机活动机翼上内侧电机所在位置固定连接,连杆的另一端与滑块连接;无人机机身前端侧面分别设置活动机翼;机翼固定端为梯形机构,机翼固定端固定设置在无人机机身前端侧面,机翼活动端和机翼固定端通过转动铰链连接;机身滑轨上的滑块带动与连杆连接的活动机翼围绕翼根处的铰链转动。
Unmanned aerial vehicle capable of vertically taking off and landing and full-wing tilting structure thereof
一种可垂直起降无人机及其全机翼倾转结构
2024-12-20
Patent
Electronic Resource
Chinese
IPC: | B64U |
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