The invention provides a rapid and repeated folding and unfolding control device for simulating a control surface, relates to the technical field of aircraft testing, and aims to solve the technical problem that a control surface simulating device cannot be folded and unfolded repeatedly. The device comprises a base, a tiller and a control surface connected with the tiller, wherein the tiller is rotationally arranged on the base; the tiller is provided with a first arc surface opposite to the control surface and further provided with a locking groove formed in the first arc surface. The device further comprises a reset element and a sliding block arranged on the base in a sliding mode. The sliding block is provided with a first protruding block and a second protruding block which are opposite to the reset element. Wherein the length of the first convex block is greater than that of the second convex block; the simulation device further comprises a stop ring hinged to the base, and the stop ring is provided with a first end and a second end. When the device is in a locking mode, the second protruding block abuts against the interior of the locking groove, and the first protruding block abuts against the second end of the stop ring. The device for simulating the control surface is compact in structure, can avoid repeated disassembly and assembly, and is high in unfolding and folding conversion speed.

    本发明提供了一种用于模拟舵面的快速重复折叠展开操纵装置,涉及飞行器测试技术领域,以解决模拟舵面装置无法重复折叠展开的技术问题。该装置包括基座、舵柄和与舵柄相连的舵面,舵柄转动设在基座;舵柄具有与舵面相对的第一圆弧面,舵柄还具有形成在第一圆弧面上的锁定槽;装置还包括复位元件以及滑动设在基座上的滑块,滑块具有与复位元件相对的第一凸块和第二凸块;其中,第一凸块的长度大于第二凸块的长度;模拟装置还包括铰接于基座的止动圈,止动圈具有第一端和第二端;当装置处在锁定模式,第二凸块止抵在锁定槽中,第一凸块抵接于止动圈的第二端。本发明的模拟舵面的装置结构紧凑,可避免重复拆装,且展开折叠转换速度快。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rapid repeated folding and unfolding control device for simulating control surface


    Weitere Titelangaben:

    一种用于模拟舵面的快速重复折叠展开操纵装置


    Beteiligte:
    WANG HAO (Autor:in) / YU DONGDONG (Autor:in) / TANG XUDONG (Autor:in) / WEI HOUZHEN (Autor:in) / WANG KAI (Autor:in) / LI ZHAOKAI (Autor:in) / LIU CHAO (Autor:in) / KOU CHENGHAO (Autor:in)

    Erscheinungsdatum :

    28.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F16C SHAFTS , Wellen / 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



    Aircraft control surface lateral folding and unfolding mechanism

    LIU XUDONG / XU YANG | Europäisches Patentamt | 2023

    Freier Zugriff

    Zero-gravity simulation follow-up device of repeated folding and unfolding mechanism

    LUO HAIJUN / PENG ZHILONG / LI FANGZHOU et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Rapid unfolding method for folding rudder blade

    KOU CHENGHAO / WANG CHAORAN / GUO HUI et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Rapid unfolding mechanism for folding rudder blade

    KOU CHENGHAO / YIN JUN / MA JUN et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    High-folding-unfolding-ratio cylindrical surface unfolding and folding mechanism with solid reflecting surface

    XIAO HANG / LYU SHENGNAN / DING JIANZHONG et al. | Europäisches Patentamt | 2025

    Freier Zugriff