The invention relates to a load releasing device and an aircraft thereof, the load releasing device comprises a releasing cabin, a heat-proof cover plate, a first releasing assembly and a second releasing assembly, a load containing cavity is formed in the releasing cabin, and an opening is formed in one end of the releasing cabin; the heat-proof cover plate is buckled on one side of the opening of the release cabin; the first release assembly is mounted on the release cabin, one end of the first release assembly is connected with the heat-proof cover plate, and the first release assembly is used for pushing the heat-proof cover plate away from the release cabin; the second releasing assembly is mounted on the releasing cabin, and one end of the second releasing assembly is attached to the load and used for driving the load to approach the opening of the releasing cabin; wherein the heat-proof cover plate is provided with a release position, and when the first release assembly pushes the heat-proof cover plate to the release position, a gap for a load to penetrate through is formed between the heat-proof cover plate and the release cabin. The heat-proof cover plate is pushed to the release position through the first release assembly, the load is pushed through the second release assembly, the load can be moved out of the release cabin, and stable release of the load of an aircraft under the high-speed and large-dynamic-pressure working condition is achieved.

    本申请涉及一种载荷释放装置及其飞行器,其包括:释放舱、防热盖板、第一释放组件和第二释放组件,释放舱内设置有载荷容置腔,释放舱一端设置有开口;防热盖板扣合于释放舱开口一侧;第一释放组件安装于释放舱上,且一端与防热盖板连接,并用于顶推防热盖板远离释放舱;第二释放组件安装于释放舱上,第二释放组件一端用于与载荷贴合,用于驱使载荷靠近释放舱开口;其中,防热盖板具有一释放位置,当第一释放组件顶推防热盖板至释放位置时,防热盖板与释放舱之间形成有用于供载荷穿设的间隙。本发明通过第一释放组件顶推防热盖板至释放位置,第二释放组件顶推载荷,使载荷可以移出释放舱内部,解决了飞行器在高速、大动压工况下载荷的稳定释放。


    Access

    Download


    Export, share and cite



    Title :

    Load releasing device and aircraft thereof


    Additional title:

    一种载荷释放装置及其飞行器


    Contributors:
    WANG PANYU (author) / ZHANG ZHENGYI (author) / XU GAOPING (author) / YONG SIWEN (author) / DAI ZHAOPENG (author)

    Publication date :

    2025-04-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



    FIXING/RELEASING METHOD OF HEAVY LOAD AND DEVICE THEREOF

    MORIWAKI KOJI / HOSOBUCHI SEIJI | European Patent Office | 2020

    Free access

    Device for releasing an aircraft panel and associated aircraft

    PENELLA DANIEL | European Patent Office | 2023

    Free access

    DEVICE FOR RELEASING AN AIRCRAFT PANEL AND ASSOCIATED AIRCRAFT

    PENELLA DANIEL | European Patent Office | 2021

    Free access

    Aircraft missile body mounting and releasing device and aircraft

    GAO YUNPENG / TIAN GANGYIN | European Patent Office | 2024

    Free access

    Underwater releasing device and releasing method thereof

    GAO CHENGFEI / MAO YUFENG / WANG YAZHOU et al. | European Patent Office | 2021

    Free access