The invention discloses a driving energy-adjustable rotary wing aircraft with a fixed wing, wherein the aircraft is characterized by comprising rotary curtain wings, rotary shafts, speed reducers, motors, a fuselage frame and the fixed wings; the two rotary shafts are symmetrically arranged on the two sides of the fuselage frame, and the axis directions of the two rotary shafts are both perpendicular to the longitudinal symmetry plane of the aircraft; the two motors arranged on the fuselage frame are decelerated through the two speed reducers arranged on the fuselage frame respectively and then drive the two rotary shafts to rotate continuously; the two rotary curtain wings are fixedly connected to the two rotary shafts respectively, each rotary curtain wing comprises a rotary frame and a curtain wing body mounted in the rotary frame, and each curtain wing body comprises a curtain wing frame and soft curtain mounted on the curtain wing frame; and coil springs and driving motors are further arranged in the curtain wing frames and used for controlling the soft curtains to unfold and contract, and the fixed wing is arranged on the fuselage frame and used for generating lift force.

    本发明公开了一种带有固定翼的两拉帘驱动能量可调旋转翼飞行器,其特征在于包括旋转帘翼、旋转轴、减速器、电动机、机身框架和固定翼,机身框架两侧对称的布置有两个旋转轴,两个旋转轴轴线方向都与飞行器纵向对称面垂直,设置在机身框架上的两个电动机分别通过设置在机身框架上的两个减速器减速后分别带动两个旋转轴连续旋转,两个旋转帘翼分别固定连接在两个旋转轴上,旋转帘翼包括旋转框架,以及安装在旋转框架内的帘翼,帘翼包括帘翼框架,以及安装在帘翼框架上的软质帘,帘翼框架内还设置有卷簧以及驱动电机,用于控制软质帘的展开和收缩,机身框架上设置有固定翼用于产生升力。


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    Title :

    Driving energy-adjustable rotary wing aircraft with fixed wing and two pull curtains


    Additional title:

    带有固定翼的两拉帘驱动能量可调旋转翼飞行器


    Contributors:
    LIAO ZHENQIANG (author) / ZHAO XUE (author) / WANG JIE (author) / SHENG SONGMEI (author) / NI DANYAN (author) / SHI YUN (author) / QIU MING (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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