The invention provides an ornithopter based on an adjustable fuselage. The ornithopter comprises a fuselage skeleton, a front wing transmission module, a rear wing transmission module, a battery module, a flight control module, a front wing, a rear wing and a steering module. The steering module comprises a rotating motor, the rotating motor is fixed to the fuselage framework, and a rotating shaft of the rotating motor is fixedly connected with the front wing transmission module. According to the ornithopter disclosed by the invention, the whole structure of the front wing can be rotated at a small angle through the rotating motor, the angle between the front wing and the whole ornithopter is changed, a certain included angle is formed, and the purpose of controlling the advancing direction of the ornithopter is achieved. According to the structure, the steering function of the ornithopter is realized by only using an additional rotating motor, and a complicated gear mechanism or a steering engine-empennage form is avoided.
本发明提供了一种基于可调机身的扑翼飞行器,包括机身骨架、前翅翼传动模块、后翅翼传动模块、电池模块、飞控模块、前翅翼、后翅翼和转向模块。转向模块包括旋转电机,旋转电机固定在机身骨架上,旋转电机的转轴与前翅翼传动模块固定连接。本发明的扑翼飞行器,可通过旋转电机将前翅翼整体结构进行小角度旋转,改变前翅翼与整体扑翼飞行器的角度,形成一定的夹角,达到控制扑翼飞行器前进方向的目的。该结构仅使用一个额外的旋转电机,即实现了控制扑翼飞行器转向的功能,避免了复杂的齿轮机构或者采用舵机‑尾翼的形式。
Flapping wing air vehicle based on adjustable fuselage
一种基于可调机身的扑翼飞行器
2024-04-09
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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