The invention belongs to the technical field of airships, and provides an adjustable projectile body hanging device suitable for a medium-low-altitude airship, which is characterized in that the lower end of an orientation adjusting mechanism is connected with a pitching adjusting mechanism; the lower end of the pitching adjusting mechanism is connected with the projectile body hanging mechanism; the orientation adjusting mechanism drives the rotating cylinder, the connecting disc and the projectile body hanging mechanism through the worm and gear mechanism, and orientation adjustment of the projectile body hanging device is achieved. The pitching adjusting mechanism realizes pitching of the projectile body hanging device through a worm and gear and driving and driven gear transmission mode; the posture stability control device is provided with an inertial navigation unit sensor and a servo motor controller, the inertial navigation unit sensor is installed on the orientation and pitching adjusting mechanism and the projectile body hanging mechanism and conducts real-time monitoring and posture data feedback on the posture of the projectile body, and the servo motor controller drives the servo motor to drive the orientation and pitching adjusting mechanism to act according to posture feedback data, and dynamic adjustment of the posture of the projectile body is achieved. The device is reasonable in design, compact in structure, high in practicability and reliability and convenient to maintain.

    本发明属于飞艇技术领域,提供一种适用于中低空飞艇可调弹体吊挂装置,其方位调整机构的下端连接俯仰调整机构;俯仰调整机构下端连接弹体吊挂机构;方位调整机构通过涡轮蜗杆机构带动旋转筒、连接盘和弹体吊挂机构,实现弹体吊挂装置方位调整;俯仰调整机构通过涡轮蜗杆和主从动齿轮传动方式,实现弹体吊挂装置俯仰;姿态稳定控制装置有惯性导航单元传感器和伺服电机控制器,惯性导航单元传感器安装在方位、俯仰调整机构以及弹体吊挂机构上,对弹体姿态进行实时监测以及姿态数据反馈,伺服电机控制器根据姿态反馈数据,驱动伺服电机带动方位与俯仰调整机构动作,实现对弹体姿态动态调整。本发明设计合理结构紧凑,实用性强可靠性高且便于维护。


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    Titel :

    Missile hanging posture stabilizing device for medium-low-altitude airship


    Weitere Titelangaben:

    一种中低空飞艇挂弹姿态稳定装置


    Beteiligte:
    LIU CHAOFENG (Autor:in) / LIU LIWU (Autor:in) / XING XIAOYUE (Autor:in) / BAI XUEQIANG (Autor:in) / LING CHEN (Autor:in) / LI XIAOLONG (Autor:in) / GUO JIE (Autor:in) / ZHANG LONG (Autor:in) / LI ZHE (Autor:in) / LIAO DAOYI (Autor:in)

    Erscheinungsdatum :

    2021-04-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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