The invention relates to the field of launchers launched by catapults or tracks, in particular to an unmanned aerial vehicle catapult boom, a launcher and a pool test system. The problem that in the prior art, the launching angle and the launching position of an unmanned aerial vehicle are limited, and the requirement for multi-attitude and multi-position launching cannot be met is solved. The unmanned aerial vehicle ejection arm frame comprises guide columns which are arranged in a left-right spaced mode, a centering supporting rod and an angle adjusting supporting rod are installed between the guide columns, the centering supporting rod is close to the front portion, the angle adjusting supporting rod is close to the rear portion, and the ends of the supporting rods are matched with the guide columns in a guiding mode. The pitch angle of the ejection arm is adjusted through the vertical position difference of the centering supporting rod and the angle adjusting supporting rod, and a supporting rod lifting driving device is arranged between the supporting rod and the corresponding guide column. Therefore, the unmanned aerial vehicle can be launched at any angle in a wide-range angle of pitching and pitching, and can also be launched at different heights, and the requirements of multi-attitude, multi-position and multi-launching-speed launching of the unmanned aerial vehicle in the test process are met.

    本发明涉及用弹射器或轨道发射的发射装置领域,具体涉及无人机弹射臂架、发射装置及水池试验系统。该发明以解决现有技术中无人机的发射角度和发射位置受限,无法实现多姿态、多位置发射的需求的问题。无人机弹射臂架包括左右间隔布置的导柱,导柱间安装有一个靠前、另一个靠后的定心支撑杆和调角支撑杆,支撑杆的端部与导柱导向配合,通过定心支撑杆和调角支撑杆安装有弹射臂,通过定心支撑杆和调角支撑杆的上下位置之差调节弹射臂的俯仰角,支撑杆与对应的导柱之间设置有支撑杆升降驱动装置。由此,无人机可在俯、仰的大范围角度内的任意角度进行发射,也可在不同高度进行发射,实现了无人机在试验过程中多姿态、多位置、多射速发射的需求。


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    Title :

    Unmanned aerial vehicle ejection boom, launching device and pool test system


    Additional title:

    无人机弹射臂架、发射装置及水池试验系统


    Contributors:
    MA WEIFENG (author) / LI QI (author) / CHEN YANWEI (author) / LIU QINGZHAO (author) / YANG WEI (author) / LIU YABIN (author) / ZHANG LIANG (author)

    Publication date :

    2025-04-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / 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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