The invention provides an oversized wingspan solar unmanned aerial vehicle free-air delivery system, and relates to the technical field of aircraft delivery, the oversized wingspan solar unmanned aerial vehicle free-air delivery system comprises an oversized wingspan solar unmanned aerial vehicle, an unmanned aerial vehicle mounting assembly and a pod, the unmanned aerial vehicle mounting assembly comprises a delivery frame, a plurality of upper flexible ropes and a plurality of lower flexible ropes, one ends of the upper flexible ropes are connected to different positions of the top of the throwing frame, the other ends of the upper flexible ropes are used for being connected with floating equipment, one ends of the lower flexible ropes are connected to different positions of the bottom of the throwing frame, the other ends of the lower flexible ropes are connected to different positions of the ultra-large wingspan solar unmanned aerial vehicle, and the pod is fixedly arranged in the throwing frame. Therefore, under the limitation of the plurality of lower flexible ropes, the super-large wingspan solar unmanned aerial vehicle can keep a certain posture. Compared with the prior art, the pod is fixed and supported through the throwing frame, so that the pod can be kept in a low force bearing state in the air flying process, structural deformation is avoided, and it is guaranteed that electrical equipment in the pod can work normally.

    本发明提供一种超大翼展太阳能无人机临空投放系统,涉及飞行器投放技术领域,包括:超大翼展太阳能无人机、无人机挂载组件和吊舱,无人机挂载组件包括:投放架、多个上部柔性绳索和多个下部柔性绳索,多个上部柔性绳索的一端连接至投放架顶部的不同位置,另一端用于连接浮空设备,多个下部柔性绳索的一端连接至投放架底部的不同位置,另一端连接至超大翼展太阳能无人机的不同位置,吊舱固定设置在投放架中。由此,在多个下部柔性绳索的限制下,超大翼展太阳能无人机能够保持一定的姿势。相比于现有技术,借助投放架来固定支撑吊舱,可以使其在临空飞行的过程中保持较低的承力状态,避免结构变形,保证吊舱内的电气设备能够正常工作。


    Access

    Download


    Export, share and cite



    Title :

    Oversized wingspan solar unmanned aerial vehicle air-free delivery system


    Additional title:

    一种超大翼展太阳能无人机临空投放系统


    Contributors:
    QIN YUMEI (author) / YAN FENG (author) / FU QIANG (author) / HE ZEQING (author) / YANG YANCHU (author) / HE XIAOHUI (author)

    Publication date :

    2023-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



    Ground sliding test equipment for large-wingspan unmanned aerial vehicle

    GENG ZHAOYANG / ZHU YUKUI / CAO XIANG et al. | European Patent Office | 2023

    Free access

    Method for releasing high-altitude balloon carrying large-wingspan unmanned aerial vehicle

    ZHANG DONGHUI / WANG LIXIANG / YANG YANCHU et al. | European Patent Office | 2020

    Free access

    Novel wingspan vehicle

    ZHANG GUOBING | European Patent Office | 2021

    Free access

    Single-wheel strut landing gear structure for large wingspan lightweight unmanned aerial vehicle

    WANG JUN / LI GUANGLIANG / WU CHAO et al. | European Patent Office | 2015

    Free access

    Wingspan-variable keel for unmanned sailboat

    CAO XIAOJIAN / QIN HONGDE / SHEN JINKUN et al. | European Patent Office | 2024

    Free access