The invention discloses an integrally-formed dual-mode unmanned aerial vehicle fuselage framework and a design process, and belongs to the field of unmanned aerial vehicles, the integrally-formed dual-mode unmanned aerial vehicle fuselage framework comprises a fuselage frame body used for installing main equipment and a circuit board, and six reinforcing rods are fixedly arranged on one side of the outer wall of the fuselage frame body. According to the unmanned aerial vehicle, a high-strength light integrated magnesium-aluminum fuselage is adopted, in order to increase the structural strength of the unmanned aerial vehicle fuselage and reduce the weight, the whole fuselage is divided into an equipment cabin, a power supply cabin and a task load pod, the equipment cabin is provided with a flight control navigation and power subsystem, and the power supply cabin is located at the gravity center position of the fuselage; the task load pod is placed below the power supply cabin, so that equipment can be conveniently located at an intervisibility position, the flight time, the load quality, the battery size and the rotor structure of the unmanned aerial vehicle can be preliminarily preset through calculation of customer requirements, the engineering target setting efficiency in the index design link is improved, and the design efficiency is improved to the maximum extent.

    本发明公开了一体成型双模无人机机身架构及设计工艺,属于无人机领域,该一体成型双模无人机机身架构及设计工艺法,包括,机身架本体,用于安装主要设备和电路板,机身架本体的外壁一侧固定设置有六个加固杆。本发明,无人机采用高强度轻型一体化镁铝机身,为增加无人机机身的结构强度、减轻重量,将整个机身分为设备舱、电源舱和任务载荷吊舱,设备舱布置飞控导航及动力子系统,电源舱位于机体重心位置,任务载荷吊舱放置在电源舱下方便于设备处于通视位置,利用对客户需求的计算,可以初步的完成对无人机飞行时间、载荷质量、电池大小和旋翼结构进行预设,提高了指标设计环节中的工程目标设定效率,最大程度提高设计的效率。


    Access

    Download


    Export, share and cite



    Title :

    Integrally-formed dual-mode unmanned aerial vehicle fuselage framework and design process


    Additional title:

    一体成型双模无人机机身架构及设计工艺


    Contributors:
    GUO JIANHUI (author) / YI PING (author) / LIU FAN (author) / XU RUFENG (author)

    Publication date :

    2022-04-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    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 / B64C AEROPLANES , Flugzeuge



    Method for integrally forming fuselage of unmanned aerial vehicle and fuselage of unmanned aerial vehicle

    TIAN XIAO / HE DANQI / YU BAIMING et al. | European Patent Office | 2024

    Free access

    Fuselage of unmanned aerial vehicle and unmanned aerial vehicle with fuselage

    LIANG JIE | European Patent Office | 2021

    Free access

    Fuselage of unmanned aerial vehicle and unmanned aerial vehicle with fuselage

    LIANG JIE / XIAO DINGFENG | European Patent Office | 2021

    Free access


    Unmanned aerial vehicle fuselage, manufacturing method and unmanned aerial vehicle with unmanned aerial vehicle fuselage

    LI JIANHUI / HOU WEIKANG / SHI XIAOFEI et al. | European Patent Office | 2024

    Free access