The invention relates to a large high-maneuverability flapping-wing aircraft capable of hovering based on a clapping effect. The flapping power system comprises a first driving motor, an electronic speed regulator, a gear mechanism and an X-shaped layout wing, two wing beams of the X-shaped layout wing are arranged in a crossed mode and are fixedly connected with a fuselage in a rotatable mode, and the two wing beams of the X-shaped layout wing are fixedly connected with the fuselage in a rotatable mode. The two wing beams are rotatably and fixedly connected with the gear mechanism through twoconnecting rods respectively, and the gear mechanism controls the two wing beams to symmetrically swing relative to the fuselage in a linkage mode through the two connecting rods respectively, so that the wings in the X-shaped layout are symmetrically arranged in a linkage mode for striking; the tail rotor wing two-way propelling system comprises a tail rotor wing, a two-way electronic speed regulator and a second driving motor, and the second driving motor drives the tail rotor wing to rotate forwards and backwards to generate yawing moment; and the energy and flight control system comprisesa lithium battery and a flight control module and is used for providing energy and data acquisition, processing and output for the aircraft. According to the aircraft, flapping effects are generatedby wing flapping, the thrust is large, the task load is large, the tail rotor wing actively controls the course, the anti-interference performance is high, and course control is effectively achieved.

    本公开涉及一种基于拍合效应的大型高机动可悬停扑翼飞行器,扑打动力系统包括驱动电机一、电子调速器、齿轮机构和X型布局机翼,X型布局机翼两根翼梁交叉布置、且分别与机身可转动固连,两根翼梁分别通过一根连杆与齿轮机构可转动固连,齿轮机构通过两根连杆分别控制两根翼梁相对于机身对称联动摆动,使X型布局机翼对称联动扑打;尾旋翼双向推进系统包括尾旋翼、双向电子调速器和驱动电机二,驱动电机二驱动尾旋翼正反双向转动,产生偏航力矩;能源与飞控系统包括锂电池、飞控模块,为飞行器提供能源以及数据的采集、处理和输出。本申请飞行器机翼扑打产生拍合效应,推力大,任务载荷大,尾旋翼主动航向控制,抗干扰性强,有效实现航向控制。


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    Title :

    Large high-maneuverability flapping-wing aircraft capable of hovering based on clapping effect


    Additional title:

    一种基于拍合效应的大型高机动可悬停扑翼飞行器


    Contributors:
    ZHAO LONGFEI (author) / WANG LIANG (author) / JIANG WUYAO (author) / JIAO ZONGXIA (author) / WANG WENSHUO (author)

    Publication date :

    2021-02-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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