The invention provides an aircraft gravity center solid-state adjusting device which comprises a guide rail fixedly connected with an aircraft structure, and continuous racks are integrated on the guide rail; the sliding mechanism is installed on the guide rail, and the sliding mechanism can move in the first direction of the guide rail; the limiting device is used for limiting the sliding mechanism to move in the second direction, and the first direction is different from the second direction; meanwhile, the invention further provides an aircraft gravity center solid-state adjusting method. By means of the device and method, the gravity center of the aircraft can be adjusted with high efficiency.

    本申请提供了一种飞行器重心固态调节装置,所述调节装置包括:导轨,与飞行器结构固定连接,所述导轨上集成有连续的齿条;滑动机构,安装于所述导轨上,所述滑动机构能够沿所述导轨的第一方向移动;限位装置,用于限制滑动机构沿第二方向运动,所述第一方向与所述第二方向不同;同时,本申请还提供了一种飞行器重心固态调节方法;本发明所述装置与方法能够以较高的效率实现飞行器重心的调节。


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    Titel :

    Solid-state adjusting device and method for gravity center of aircraft


    Weitere Titelangaben:

    一种飞行器重心固态调节装置和方法


    Beteiligte:
    YAN PENGQING (Autor:in) / HUI YUE (Autor:in) / ZHAO ZHEN (Autor:in) / LYU WENJIE (Autor:in) / LIU JIAJIA (Autor:in) / HAN CHENXING (Autor:in) / NIU YAHONG (Autor:in)

    Erscheinungsdatum :

    01.03.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / 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



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