The invention provides an unmanned aerial vehicle modularized nose and fuselage connecting structure and an unmanned aerial vehicle with the unmanned aerial vehicle, the unmanned aerial vehicle modularized nose and fuselage connecting structure comprises a nose assembly and a fuselage assembly, the nose assembly comprises a nose skin, a bulkhead, a reinforcing rib and an equipment plate, and the reinforcing rib is fixedly arranged on the nose skin on the inner side of the nose assembly in the length direction of the nose assembly; the reinforcing ribs protrude out of the end face of the partition frame, the machine head skin comprises a first glass fiber layer, a second glass fiber layer and an aramid paper honeycomb layer, the partition frame comprises a first carbon fiber layer and a first PMI foam layer, the machine body assembly comprises a reinforcing frame and a machine body skin, the machine body skin is laid on the outer side of the reinforcing frame, and the reinforcing frame is provided with reinforcing rib grooves. The reinforcing ribs are matched with the reinforcing rib grooves so that the machine head assembly can be connected with the machine body assembly. By means of the technical scheme, the technical problems that in the prior art, when the nose is mounted and dismounted, the workload is large, the process is tedious, the battle preparation time is long, and the unmanned aerial vehicle cannot make a quick response to the wartime requirement easily are solved.

    本发明提供了一种无人机模块化机头机身连接结构及具有其的无人机,包括机头组件和机身组件,机头组件包括机头蒙皮、隔框、加强筋和设备板,加强筋沿机头组件的长度方向固定设置在机头组件的内侧机头蒙皮上,加强筋凸出于隔框的端面设置,机头蒙皮包括第一玻璃纤维层、第二玻璃纤维层和芳纶纸蜂窝层,隔框包括第一碳纤维层和第一PMI泡沫层,机身组件包括加强框和机身蒙皮,机身蒙皮敷设在加强框外侧,加强框具有加强筋凹槽,加强筋与加强筋凹槽相配合以实现机头组件与机身组件相连接。应用本发明的技术方案,以解决现有技术中机头安装和拆卸时工作量大、过程繁琐、作战准备时间较长,不利于无人机对战时需求作出快速响应的技术问题。


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    Titel :

    Modular nose and fuselage connecting structure of unmanned aerial vehicle and unmanned aerial vehicle with modular nose and fuselage connecting structure


    Weitere Titelangaben:

    无人机模块化机头机身连接结构及具有其的无人机


    Beteiligte:
    WANG FEIFEI (Autor:in) / LI SHANG (Autor:in) / HUANG CHENGJING (Autor:in)

    Erscheinungsdatum :

    2024-01-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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