The invention relates to the technical field of ornithopters, in particular to an ornithopter flapping wing form adjusting structure device which comprises a plurality of main frameworks, a plurality of auxiliary frameworks and a plurality of wing edge plates, and angle adjustment can be achieved between the corresponding main frameworks, between the main frameworks and the auxiliary frameworks and between the auxiliary frameworks. The corresponding main frameworks are fixedly connected with the wing edge plates, and the corresponding auxiliary frameworks are hinged or fixedly connected with the wing edge plates. The flapping wing is reasonable in structure, angle change of the main framework, the auxiliary framework and the wing edge plate is achieved through stretching and retracting of the telescopic blocks, the flapping wing can achieve self shape change, wing waving flight of birds and the like is better simulated, the better bionic effect is achieved, and therefore the aerodynamic performance of an aircraft is improved; the flight efficiency and the flight flexibility and stability are improved, so that more complex flight actions can be completed, and the requirement of executing various high-difficulty tasks in various different complex environments can be met.
本发明涉及扑翼飞行器技术领域,具体是指一种扑翼飞行器扑翼形态的调整结构装置,包括若干主骨架、若干副骨架和若干翼边板,对应的主骨架与主骨架之间、主骨架与副骨架之间、副骨架与副骨架之间能够实现角度调节,对应的主骨架与翼边板之间固定连接、对应的副骨架与翼边板之间铰接或固定连接。本发明结构合理,通过伸缩块的伸缩,实现主骨架、副骨架及翼边板件的的角度变化,使得扑翼能够实现自身的形态变化,更好模拟如鸟类的挥动翅膀飞行,具有更好的仿生效果,从而提高飞行器的气动性能,提高飞行效率以及飞行的灵活性和稳定性,使其能够完成更加复杂的飞行动作,以满足在各种不同复杂环境下能够执行各种高难度任务的需求。
Adjusting structure device for flapping wing form of flapping wing air vehicle
一种扑翼飞行器扑翼形态的调整结构装置
2024-06-25
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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