The invention relates to the field of unmanned aerial vehicle equipment, in particular to a reconnaissance and attack integrated unmanned aerial vehicle which comprises an unmanned aerial vehicle body, wherein main wings are fixedly installed at the upper end of the unmanned aerial vehicle body through bolts, and two ailerons are arranged at the rear end of the unmanned aerial vehicle body; the two ailerons are matched with the main wing to form a triangular section; three paddles are installed at the tail end of the unmanned aerial vehicle body, and the included angle formed between every two adjacent paddles is 120 degrees; and the unmanned aerial vehicle body is internally provided with a motor and a battery, the front end of the unmanned aerial vehicle body is provided with a pan-tilt camera and an airspeed tube, the lower end of the front side of the unmanned aerial vehicle body is provided with a supporting assembly, and the lower end of the rear side of the unmanned aerial vehicle body is provided with a landing assembly. According to the reconnaissance and attack integrated unmanned aerial vehicle, a triangle is formed at the lower end of the whole unmanned aerial vehicle body through the cooperation of the landing assembly and the supporting assembly, and the triangle has stability, so that the reconnaissance and attack integrated unmanned aerial vehicle has good stability during placement, takeoff and taxiing.
本发明涉及无人机设备领域,具体是一种察打一体无人机,包括:无人机本体,所述无人机本体上端通过螺栓安装固定有主翼,无人机本体后端设有副翼,副翼的数量为两个;两个副翼与主翼配合作用形成三角形截面;所述无人机本体末端安装有桨叶,桨叶的数量为三个,相邻两个桨叶之间形成的夹角为120°;所述无人机本体内部设有电机以及电池,无人机本体前端设有云台相机与空速管,无人机本体前侧下端安装有支撑组件,无人机本体后侧下端设有起落组件;所述的察打一体无人机通过设置的起落组件与支撑组件配合作用在整个无人机本体下端形成三角形,三角形具备稳定性,因此在所述察打一体无人机放置以及起飞滑行时均具备较好的稳定性。
Reconnaissance and attack integrated unmanned aerial vehicle
一种察打一体无人机
2021-12-21
Patent
Electronic Resource
Chinese
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