The invention provides an active coaxial efficient rotor system. The active coaxial efficient rotor system comprises a rotor wheel (1) and a duct (2), wherein the rotor wheel (1) comprises blades (11), an impeller (12), a permanent magnet array (13), an active adjusting winglet (16) and a distance sensing probe (17); the permanent magnet array (13) and the distance sensing probe (17) are arranged on the impeller (12) along the circumference; the duct (2) comprises a suspension groove (21), a coil array (22) and a distance sensor (24); the coil array (22) and the distance sensor (24) are arranged on the suspension groove (21) along the circumference; and an active adjusting winglet (16) is arranged at the wing-shaped tail end of the blade (11) and is used for rotating according to a detection result of the distance sensor (24) on the distance sensing probe (17), so that the rotor wheel (1) is positioned in the center of the suspension groove (21). The weight can be reduced, pneumatic blockage is reduced, and the pneumatic efficiency is improved.

    本发明提供一种主动同轴高效旋翼系统,包括:旋翼轮(1)和涵道(2);旋翼轮(1)包括:叶片(11)、叶轮(12)、永磁阵列(13)、主动调节小翼(16)和距离感应探头(17);永磁阵列(13)和距离感应探头(17)沿圆周布置在叶轮(12)上;涵道(2)包括:悬浮槽(21)、线圈阵列(22)和距离传感器(24);线圈阵列(22)和距离传感器(24)沿圆周布置在悬浮槽(21)上;叶片(11)的翼型尾端设置有主动调节小翼(16),主动调节小翼(16)用于根据距离传感器(24)对距离感应探头(17)的检测结果转动,使得旋翼轮(1)位于悬浮槽(21)中心。可减轻重量,并且减小气动阻塞,提高气动效率。


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    Titel :

    Active coaxial efficient rotor system


    Weitere Titelangaben:

    一种主动同轴高效旋翼系统


    Beteiligte:
    LIU YANTAO (Autor:in)

    Erscheinungsdatum :

    2022-02-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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