The invention discloses an unpowered micro aircraft launching device based on multi-stage acceleration. The unpowered micro aircraft launching device comprises a lead screw bouncing mechanism, a multi-stage acceleration mechanism, a limiting mechanism and other mechanisms. The screw rod bomb-up mechanism is arranged at the top end of the rear part of the frame and is used for pushing the unpowered micro aircraft to continuously bomb up to the multi-stage acceleration mechanism; the multi-stage acceleration mechanism is arranged at the front part of the frame and is used for accelerating the launching of the unpowered micro aircraft pushed by the screw rod missile-loading mechanism; the limiting mechanisms are distributed on the frame, the lead screw missile-loading mechanism and the multi-stage acceleration mechanism and used for limiting the position of the unpowered micro aircraft and guaranteeing stable and continuous missile-loading launching of the unpowered micro aircraft. The launching function of shooting at a constant speed of the micro aircraft is achieved, the launching effect is more stable, and the service life of the device is longer; the device can load four or more micro aircrafts at a time, and the launching efficiency is high.

    本发明公开了一种基于多级加速的无动力微型飞行器发射装置,包括丝杆上弹机构、多级加速机构、限位机构等机构;丝杆上弹机构设置在框架后部的顶端,用于推动无动力微型飞行器向多级加速机构的连续上弹;多级加速机构设置在框架的前部,用于加速发射经过丝杆上弹机构推送来的无动力微型飞行器;限位机构分布设置在框架、丝杆上弹机构和多级加速机构上,用于限制无动力微型飞行器的位置并保证无动力微型飞行器的稳定连续上弹发射。实现了微型飞行器以恒定速度射击的发射功能,发射效果更加稳定,装置使用寿命更长;本装置可一次性装载四个及以上的微型飞行器,发射效率高。


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    Title :

    Unpowered micro aircraft launching device based on multi-stage acceleration


    Additional title:

    一种基于多级加速的无动力微型飞行器发射装置


    Contributors:
    ZHUANG CHENYUE (author) / HU TAO (author)

    Publication date :

    2023-08-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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