The invention discloses a coaxial double-propeller aircraft based on side wing flight control. The coaxial double-propeller aircraft comprises a fuselage, a coaxial double-propeller lift mechanism and a plurality of attitude adjusting mechanisms uniformly distributed on the periphery of the fuselage, the coaxial double-paddle lift mechanism is mounted on the fuselage and comprises a forward paddle, a reverse paddle and a lift motor, and the lift motor can simultaneously drive the forward paddle to rotate forward and the reverse paddle to rotate reversely; the posture adjusting mechanism comprises a first motor, a second motor and a side wing, the first motor can drive the side wing to be close to or away from the surface of the fuselage, and the second motor can drive the side wing to block downward airflow generated by the forward propeller and the backward propeller at different angles. While the size of the aircraft is reduced, the aircraft is ensured to have good maneuverability.

    本发明公开了一种基于侧翼飞控的共轴双桨飞行器,包括:机身、共轴双桨升力机构和多个均布在机身外周的姿态调整机构;所述共轴双桨升力机构安装在机身上,所述共轴双桨升力机构包括正桨、反桨和升力电机,所述升力电机能够同时驱动正桨正转和反桨反转;所述姿态调整机构包括第一电机、第二电机和侧翼,所述第一电机能够带动所述侧翼靠近和远离机身表面,所述第二电机能够带动所述侧翼以不同角度阻挡正桨和反桨产生的向下的气流。在缩小飞行器体积的同时,确保飞行器具有良好的可操纵性。


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    Title :

    Coaxial double-propeller aircraft based on side wing flight control


    Additional title:

    一种基于侧翼飞控的共轴双桨飞行器


    Contributors:
    WANG ZHIQIANG (author) / SUN XIAODONG (author) / WU TIANLONG (author) / XU CHANGMING (author)

    Publication date :

    2024-05-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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