The invention discloses a dynamic variable wing bionic aircraft which comprises a fuselage assembly, a speed reducing mechanism, a wing assembly, a wing vein driving assembly, an empennage assembly, a receiver and a battery, the fuselage assembly comprises a nose and a fuselage plate, the nose and the fuselage plate are connected to form a nose cavity, and the fuselage plate is provided with the fuselage cavity, a first groove and a second groove; the wing assembly is arranged on the fuselage plate; the speed reducing mechanism is arranged in the nose cavity and is used for driving the wing assembly to flap up and down; the wing vein driving assembly is arranged in the first groove of the fuselage plate and used for driving the wing assembly to move transversely and longitudinally; the empennage assembly is arranged at the tail part of the fuselage plate and can turn over and move up and down; the receiver is arranged in a machine body cavity of the machine body plate; and the battery is arranged in the second groove of the machine body plate. According to the dynamic variable-wing bionic aircraft, the structural state of the wings can be adjusted in the flying process, and the shape of the wings can be adjusted in real time to achieve the optimal flying state.

    本发明公开了一种动态变翅翼仿生飞行器,包括机身组件、减速机构、翅翼组件、翅脉驱动组件、尾翼组件、接收器和电池,所述机身组件包括机头和机身板,所述机头与机身板连接形成机头腔,所述机身板上设有机身腔、第一凹槽和第二凹槽;所述翅翼组件设置在机身板上;所述减速机构设置在机头腔内,用于驱动翅翼组件上下扑动;所述翅脉驱动组件设置在机身板的第一凹槽内,用于驱动翅翼组件横纵向移动;所述尾翼组件设置在机身板的尾部,上下翻转运动;所述接收器设置在机身板的机身腔内;所述电池设置在机身板的第二凹槽内。本发明动态变翅翼仿生飞行器在飞行的过程中可以调整翅翼的结构状态,且能够实时调整翅翼的形状来达到最佳飞行状态。


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    Title :

    Dynamic variable wing bionic aircraft


    Additional title:

    动态变翅翼仿生飞行器


    Contributors:
    HE GANG (author) / YANG HU (author) / HAN ZHENGTONG (author) / SUN JINHAO (author) / ZHU FENG (author) / CHEN XUAN (author)

    Publication date :

    2023-06-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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