The invention discloses a high aspect ratio wing follow-up loading device, which comprises a force direction control assembly, a displacement control assembly, a position monitoring assembly and a servo control assembly, and is characterized in that the force direction control assembly comprises a clamping plate, a pull pressure sensor, a connecting rod and a spherical hinge, and the clamping plate is clamped and fixed on a load loading point of a high aspect ratio wing; the connecting rod is connected with the tension-pressure sensor and the spherical hinge; the displacement control assembly comprises a connecting ring, an electric servo cylinder and a lead screw linear sliding table. The position monitoring assembly comprises a vertical displacement sensor and a horizontal displacement sensor. And the servo control assembly performs movement control on the lead screw linear sliding table according to the displacement detected by the two displacement sensors until a force value displayed by the tension and pressure sensor is a calibration force value, so that follow-up loading of the high-aspect-ratio wing is realized. According to the invention, follow-up loading of the high-aspect-ratio wing can be realized, the requirement on a laboratory site is reduced, and the risk in the test process is reduced.

    本发明公开了一种大展弦比机翼随动加载装置,包括力方向控制组件、位移控制组件、位置监测组件和伺服控制组件,力方向控制组件包括夹持卡板、拉压力传感器、连接杆、球铰,夹持卡板夹持并固定于大展弦比机翼的载荷加载点上,连接杆连接拉压力传感器与球铰;位移控制组件包括连接环、电动伺服缸和丝杠直线滑台;位置监测组件包括竖直位移传感器和水平位移传感器;伺服控制组件根据两个位移传感器检测的位移,对丝杠直线滑台进行移动控制,直至拉压力传感器显示的力值为标定力值,从而实现大展弦比机翼的随动加载。本发明能够实现大展弦比机翼的随动加载,减小对实验室场地的要求,降低试验过程中的风险。


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    Titel :

    High-aspect-ratio wing follow-up loading device


    Weitere Titelangaben:

    一种大展弦比机翼随动加载装置


    Beteiligte:
    GUO CAIGUOHUI (Autor:in) / YANG JUN (Autor:in) / TIAN YONGWEI (Autor:in) / WANG YONG (Autor:in) / QI HEYANG (Autor:in) / NI TIANQI (Autor:in)

    Erscheinungsdatum :

    13.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen






    Thick high aspect ratio wing, part 2

    Erickson, L. L. / Gambucci, B. J. / Wilcox, P. R. | NTRS | 1971


    Wing follow-up deformation loading device

    YANG RUI / ZHANG KAIHANG / WEI LEI et al. | Europäisches Patentamt | 2022

    Freier Zugriff