The invention provides a fixed-wing aircraft wing docking system and method, and relates to a wing docking technology. The system comprises a movable platform; a multi-degree-of-freedom platform, which is connected to the upper portion of the movable platform, wherein an outer wing butt joint structure and a fixed wing butt joint structure are connected to the upper portion of the multi-degree-of-freedom platform, an outer wing is located on an outer wing butt joint structure, and a fixed wing is located on a fixed wing butt joint structure; and a control end, which is connected with and controls the movable platform, the multi-degree-of-freedom platform, the outer wing butt joint structure and the fixed wing butt joint structure to work. Butt joint accidents are reduced, and the butt joint efficiency is improved.

    本发明提供一种固定翼飞行器机翼对接系统及方法,涉及机翼对接技术,包括:移动平台;多自由度平台,连接于所述移动平台上方,所述多自由度平台上方连接有外翼对接结构和固定翼对接结构,外翼位于所述外翼对接结构上,固定翼位于所述固定翼对接结构上;控制端,连接并控制所述移动平台、所述多自由度平台、所述外翼对接结构和所述固定翼对接结构工作,减少对接事故的发生,并提高对接的效率。


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    Title :

    Fixed-wing aircraft wing docking system and method


    Additional title:

    一种固定翼飞行器机翼对接系统及方法


    Contributors:
    DU YIZHEN (author) / LIU YUAN (author) / GONG BINJUN (author)

    Publication date :

    2021-09-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    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



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