The invention provides an intelligent airfoil profile and a rotor wing, the intelligent airfoil profile comprises an I-shaped pipe 6, a U-shaped pipe 5, a cross beam 7, a flexible skin 4 and a fuel oil medium 9, the cross beam 7 is located in the middle of the whole airfoil profile, and the center of the cross beam 7 is matched with the gravity center of the whole airfoil profile; the flexible skin 4 is arranged on the outer contour of the whole intelligent airfoil; the wing-shaped space inside the flexible skin 4 and the first-layer concave pipe 5 on the flexible skin 4 and outside the cross-shaped beam 7 and the first-layer concave pipe 5 on the cross-shaped beam 7 is filled with the I-shaped pipe 6 in a combined mode, and the gap space outside the I-shaped pipe 6 is filled with the fuel oil medium 9; the I-shaped pipe 6 comprises an I-shaped beam 1 and two flexible half pipes 2; the N I-shaped pipes form three combination types, namely a crisscross uniform distribution combination 8, a longitudinal arrangement combination 10 and a transverse arrangement combination 11; the concave pipe 5 comprises a concave beam 3 and a flexible half pipe 2; the flexible half pipes of the I-shaped pipe and the U-shaped pipe are filled with fuel oil media. The flexible half pipe 2 comprises an arc-shaped edge and a right-angle edge.

    本申请提供一种智能翼型及旋翼,所述智能翼型包括:工字管6、凹字管5、十字梁7、柔性蒙皮4、燃油介质9,其中:十字梁7位于整个翼型的中间位置,十字梁7中心与整个翼型的重心吻合;柔性蒙皮4布置在整个智能翼型的外轮廓;柔性蒙皮4及其上的第一层凹字管5以内,十字梁7及其上的第一层凹字管5以外的翼型空间,使用工字管6进行组合填充,工字管6外的间隙空间,使用燃油介质9填充;工字管6包括工字梁1和2个柔性半管2;N个工字管构成三种组合类型,即纵横交叉均布组合8、纵列排布组合10、横列排布组合11;凹字管5包括凹字梁3和1个柔性半管2;工字管和凹字管的柔性半管内部均填充燃油介质;柔性半管2包括弧形边和直角边。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Intelligent airfoil profile and rotor wing


    Weitere Titelangaben:

    一种智能翼型及旋翼


    Beteiligte:
    LI JINSHENG (Autor:in) / ZHANG HAOFU (Autor:in) / LI JINGJING (Autor:in) / WANG XIN (Autor:in) / CHEN JUN (Autor:in) / CHEN CHANGHUA (Autor:in) / SONG LINQING (Autor:in)

    Erscheinungsdatum :

    17.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Wing with deformable and reconfigurable airfoil profile

    JING MENGKAI / MENG FANQIANG / ZHANG XINZHAO et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    WING AIRFOIL

    PETROV ALBERT VASILEVICH / STEPANOV JURIJ GEORGIEVICH / POTAPCHIK ALEKSANDR VLADIMIROVICH et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    Rotor and Airfoil Design for Efficient Rotary Wing Micro Air Vehicles

    Bohorquez, F. / Pines, D. J. / American Helicopter Society | British Library Conference Proceedings | 2005


    Pivoting wing as sub-airfoil-pivoting wing with pivotable sub-airfoil

    FRANK KARGER | Europäisches Patentamt | 2025

    Freier Zugriff

    AIRFOIL WING-SHAPED AIRCRAFT

    CHO HYUNG HEE / CHOI SEUNGYEONG / KIM JIHYUK et al. | Europäisches Patentamt | 2022

    Freier Zugriff