The invention provides an unmanned aerial vehicle integral oil tank and an unmanned aerial vehicle with the same. The oil tank is made of metal. The fuel tank is divided into a fuel tank front section and a fuel tank rear section by taking the wing front frame as a boundary, the fuel tank front section comprises a fuel tank front frame, a wing front frame, a front longitudinal beam and a fuel tank front section skin assembly, the fuel tank front frame, the wing front frame and the front longitudinal beam form a framework of the fuel tank front section, and the fuel tank front section skin assembly covers the framework; the fuel tank rear section comprises a wing front frame, a wing rear frame, a fuel tank rear frame, a rear longitudinal beam, a fuel tank cover plate, a boosting short beam and a fuel tank rear section skin assembly, the wing front frame, the wing rear frame, the fuel tank rear frame and the rear longitudinal beam form a frame of the fuel tank rear section, and the fuel tank rear section skin assembly covers the frame to ensure the fuel tightness of the fuel tank rear section; the boosting short beam is installed between the wing rear frame and the fuel tank rear frame and attached to the fuel tank rear section skin. The unmanned aerial vehicle can bear harsh loads during large-overload maneuvering flight of the unmanned aerial vehicle and rocket boosting launching.

    本发明提供一种无人机整体式油箱及具有其的无人机,油箱为金属制成;油箱以机翼前框为分界分为油箱前段、油箱后段,油箱前段包括油箱前框、机翼前框、前纵梁和油箱前段蒙皮组件,油箱前框、机翼前框和前纵梁组成油箱前段的框架,箱前段蒙皮组件覆盖在框架上,油箱后段包括机翼前框、机翼后框、油箱后框、后纵梁、油箱盖板、助推短梁和油箱后段蒙皮组件,机翼前框、机翼后框、油箱后框、后纵梁组成油箱后段的框架,油箱后段蒙皮组件覆盖在框架上,保证油箱后段油密,助推短梁安装在机翼后框与油箱后框之间,和油箱后段蒙皮贴合。本发明能够承受无人机大过载机动飞行以及火箭助推发射时的严酷载荷。


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    Titel :

    Unmanned aerial vehicle integral oil tank and unmanned aerial vehicle with same


    Weitere Titelangaben:

    一种无人机整体式油箱及具有其的无人机


    Beteiligte:
    LI JIANHUI (Autor:in) / HE LIJUN (Autor:in) / SHI XIAOFEI (Autor:in) / CHANG HAO (Autor:in) / TIAN XINFENG (Autor:in) / HOU WEIKANG (Autor:in) / YAO YUNFENG (Autor:in) / WEI CHANGQUAN (Autor:in)

    Erscheinungsdatum :

    29.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / B64U



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