The invention discloses a driving energy-adjustable continuous winged device with variable windward area and variable dip angle, wherein the device comprises a belt wing, a slide way and a connecting piece; the belt wing is connected to the connecting piece and can rotate relatively, the connecting piece is connected to the slide way in a sliding mode, the slide way is arranged on an aircraft, and the belt wing comprises a belt wing frame and a soft belt mounted on the belt wing frame; and large belt wheels, small belt wheels, tensioning wheels and driving motors are further arranged in the winged frame and used for switching between the working state and the reset state of the belt wing. Compared with the prior art, the invention has the characteristics of small reset stroke resistance, large and stable working stroke thrust, high aerodynamic efficiency, capability of simultaneously adjusting lift force and thrust, simpler device structure and convenience in manufacturing, and can be widely applied to various small aircrafts and unmanned aerial vehicles with low Reynolds number flight.

    本发明公开了一种变迎风面积变倾角驱动能量可调连续带翼装置,包括带翼、滑道和连接件,带翼连接在连接件上且可相对转动,连接件滑动连接在滑道上,滑道设置在飞行器上,带翼包括带翼框架,以及安装在带翼框架上的软质带,带翼框架内还设置有大小带轮、张紧轮以及驱动电机,用于带翼工作状态与复位状态的切换。本发明与现有技术相比,具有复位行程阻力小、工作行程推力大且稳定、气动效率高、能同时调节升力和推力、装置结构较简单、制造方便的特点,可广泛应用于低雷诺数飞行的各类小型飞行器和无人机。


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    Title :

    Driving energy-adjustable continuous winged device with variable windward area and variable dip angle


    Additional title:

    变迎风面积变倾角驱动能量可调连续带翼装置


    Contributors:
    XUE YAN (author)

    Publication date :

    2022-01-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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