The invention discloses an aircraft connecting mechanism capable of realizing formation aggregation and separation and a control method thereof. The aircraft connecting mechanism comprises a movable gripper device and a telescopic shaft sleeve device, the movable gripper device comprises an external sleeve part fixedly connected with the aircraft host wings, an internal telescopic part which is arranged in the external sleeve part in a penetrating manner and can stretch and retract back and forth along the external sleeve part, and a first driving mechanism for driving the internal telescopic part to move back and forth; the movable gripper is located at the front end of the internal telescopic part; the second driving mechanism is used for driving the movable gripper to open and close; the telescopic shaft sleeve device comprises a sleeve fixedly connected with an aircraft slave wing, a telescopic shaft which is arranged in the sleeve in a penetrating manner and can stretch and retract back and forth along the sleeve, and a third driving mechanism for driving the telescopic shaft to move back and forth; two aircrafts in the formation are locked through linkage of the movable grippers and the telescopic shafts, and the aircrafts are pulled close or pushed away through the telescopic shafts to be gathered or separated. The method can improve the overall task flexibility and aerodynamic efficiency of the formation, and does not affect the flight quality of aircrafts.

    本发明公开了一种可实现编队聚合和分离的飞行器连接机构及其控制方法包括可动抓手装置和伸缩轴套装置,可动抓手装置包括与飞行器主机机翼相固连的外部套件、穿设在外部套件内且可沿着外部套件前后伸缩的内部伸缩件、用于驱动内部伸缩件前后运动的第一驱动机构、位于内部伸缩件前端的可动抓手以及用于驱动可动抓手开合的第二驱动机构;伸缩轴套装置包括与飞行器从机机翼相固连的套筒、穿设在套筒内且可沿着套筒前后伸缩的伸缩轴以及用于驱动伸缩轴前后运动的第三驱动机构;编队中的两架飞行器通过可动抓手与伸缩轴的链接完成锁定,利用伸缩轴拉近或推离飞行器完成聚合或分离。本发明可提高编队整体任务灵活性和气动效率,不影响飞行器飞行品质。


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    Titel :

    Aircraft connecting mechanism capable of realizing formation aggregation and separation and control method thereof


    Weitere Titelangaben:

    可实现编队聚合和分离的飞行器连接机构及其控制方法


    Beteiligte:
    YAO LINGLONG (Autor:in) / ZHANG WEILIN (Autor:in) / SHI ZHIWEI (Autor:in) / CHEN YIFEI (Autor:in) / ZHANG WEIYUAN (Autor:in)

    Erscheinungsdatum :

    2023-05-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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