The invention relates to an efficient lift flapping wing, an imitated dragonfly aircraft and an aircraft flight attitude control method. The efficient lift flapping wing comprises a flapping wing main body and a plurality of one-way air door blades, a plurality of ventilation openings are formed in the flapping wing main body, the ventilation openings are covered with the one-way air door blades respectively, and the one-way air door blades are used for enabling air flow to pass through the ventilation openings only in a one-way mode. The efficient lift flapping wing, the dragonfly-imitating aircraft and the aircraft flight attitude control method have the advantages of being high in lift providing efficiency, capable of reducing the flapping wing burden and improving the service life and stability of the aircraft.

    本发明涉及一种高效升力扑翼、仿蜻蜓飞行器及飞行器飞行姿态控制方法。本发明所述的高效升力扑翼包括:扑翼主体和若干单向风门叶片;所述扑翼主体上设有若干通风口,各所述单向风门叶片分别盖设所述通风口,所述单向风门叶片用于使气流只能单向通过所述通风口。本发明所述的高效升力扑翼、仿蜻蜓飞行器及飞行器飞行姿态控制方法具有提供升力效率高,能够降低扑翼负担,提高飞行器寿命和稳定度的优点。


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    Title :

    Efficient lift flapping wing, simulated dragonfly aircraft and aircraft flight attitude control method


    Additional title:

    一种高效升力扑翼、仿蜻蜓飞行器及飞行器飞行姿态控制方法


    Contributors:
    LIU YONGCHU (author) / LIU YUFEI (author) / HUANG JIAHUI (author)

    Publication date :

    2025-04-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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