The invention discloses a bionic aircraft which comprises an aircraft body, wings, empennages, a wing driving mechanism and an empennage driving mechanism; an accommodating cavity is defined in the aircraft body; a first opening and a second opening communicated with the accommodating cavity are formed in the aircraft body; the wings are arranged on the two sides of the aircraft body; the empennages are arranged on the two sides of the aircraft body; the empennages on the two sides are located behind the wings on the two sides respectively; the front ends of the empennages on the two sides areconnected to the second opening; the distance between the empennages on the two sides is gradually increased in an upward direction; the wing driving mechanism is arranged in the accommodating cavity, partially extends out of the first opening, is connected with the wings on the two sides and is used for driving the wings on the two sides to flap up and down in a reciprocating manner; the empennage driving mechanism is arranged in the aircraft body, is connected with the empennages on the two sides and is used for driving the empennages on the two sides to swing relative to the aircraft body.The bionic aircraft is high in flight speed and large in effective load, and can play various roles in reconnaissance, rescue and the like in various scenes.

    本发明公开了一种仿生飞行器,仿生飞行器包括:机身,机身具有容腔,机身上设有与容腔连通的第一开口和第二开口;机翼,机翼设在机身的两侧;尾翼,尾翼设在机身的两侧,两侧的尾翼分别位于两侧的机翼的后方,两侧尾翼的前端连接至第二开口,且两侧尾翼在向上方向上距离逐渐增加;机翼驱动机构,机翼驱动机构设在容腔内,机翼驱动机构部分伸出第一开口且与两侧的机翼相连,用于带动两侧的机翼上下往复扑动;尾翼驱动机构,尾翼驱动机构设在机身内,尾翼驱动机构与两侧的尾翼相连,用于带动两侧的尾翼相对机身摆动。本发明仿生飞行器飞行速度快,有效载荷大,能够在各种场景下发挥侦察、救险和其他各种作用。


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    Title :

    Bionic aircraft


    Additional title:

    仿生飞行器


    Contributors:
    ZHAO XIAOWEI (author) / ZENG DONGHONG (author) / BAOYINHEXI (author)

    Publication date :

    2020-09-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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