The invention relates to the technical field of aircrafts, in particular to a horizontal flapping wing low-altitude aircraft which comprises a rack, a nose is arranged at the front end of the rack, apropelling device is arranged at the tail end of the rack, and a first flight unit, a second flight unit and a third flight unit are sequentially arranged between the nose and the propelling device. The second flight unit is arranged in the center between the first flight unit and the third flight unit and arranged at the gravity center of the rack, a control circuit is arranged on the rack, the first flight unit, the second flight unit and the third flight unit are controlled through the control circuit, and the first flight unit and the third flight unit ascend and descend synchronously. Andthe second flight unit performs up-and-down staggered lifting action. By the adoption of the structural arrangement, under the matching action of the first flight unit, the second flight unit and thethird flight unit, lift force is generated to achieve takeoff of the aircraft, advancing is achieved under the action of the propelling device, and the aircraft is compact in structure, low in cost and capable of achieving the low-altitude flight effect.
本发明涉及飞行器技术领域,特指一种平拍翼低空飞行器,包括机架,机架前端设有机头,机架尾端设有推进装置,机头与推进装置之间依次设有第一飞行单元、第二飞行单元与第三飞行单元,第二飞行单元设于第一飞行单元与第三飞行单元之间的中心位置,且设于机架的重心位置,机架上设有控制电路,第一飞行单元、第二飞行单元与第三飞行单元分别通过控制电路控制,第一飞行单元与第三飞行单元同步升降动作,并与第二飞行单元上下交错升降动作。采用这样的结构设置,通过第一飞行单元、第二飞行单元与第三飞行单元之间的配合作用下,产生升力实现飞行器的起飞,并在推进装置的作用下实现前行,其结构紧凑,成本低,可以实现低空飞行的效果。
Horizontal flapping wing low-altitude aircraft
一种平拍翼低空飞行器
2021-03-02
Patent
Electronic Resource
Chinese
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