The invention relates to the technical field of aircrafts, in particular to a variable-attack-angle double-section flapping-wing aircraft which comprises an aircraft body, a power source and driving system, a double-section-wing flapping system left wing, a double-section-wing flapping system right wing, an attack angle adjusting driving system and an empennage adjusting driving system. Wherein the fuselage serves as a main body structure of the aircraft and is used for supporting and fixing other functional modules; the power source and the driving system are mounted on the fuselage and are used for providing power for the flapping wing to move; a left wing and a right wing of the double-section wing flapping system are mounted on the power source and the driving system.According to the variable-attack-angle double-section flapping-wing aircraft, in the flapping-wing flight process, by adjusting the attack angles of the wings in real time, the lift force and resistance distribution of the aircraft in different flight states can be optimized, and therefore the flight efficiency and stability are improved; the variable attack angle design enables the aircraft to better cope with a complex airflow environment.
本发明涉及飞行器技术领域,具体的是一种可变攻角双段扑翼飞行器,本发明包括机身、动力源及驱动系统、双段翼扑动系统左翼、双段翼扑动系统右翼、攻角调节驱动系统以及尾翼调节驱动系统;其中,机身作为飞行器的主体结构,用于支撑和固定其他功能模块;动力源及驱动系统安装于机身上,用于提供扑翼运动的动力;双段翼扑动系统左翼和右翼安装于动力源及驱动系统上,本发明提出的可变攻角双段扑翼飞行器,在扑翼飞行中,通过实时调节机翼攻角,能够优化飞行器在不同飞行状态下的升力和阻力分布,从而提高飞行效率和稳定性;可变攻角设计使飞行器能够更好地应对复杂气流环境。
Variable-attack-angle double-section flapping-wing air vehicle
一种可变攻角双段扑翼飞行器
2025-05-02
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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