The invention provides an unmanned aerial vehicle stealth leading edge and an unmanned aerial vehicle. The unmanned aerial vehicle stealth leading edge comprises a leading edge framework assembly. The integrated front edge skin is arranged on the front edge framework in the length direction of the front edge framework, and the integrated front edge skin is used for forming a front edge aerodynamic configuration and serving as an electronic reconnaissance antenna for reconnaissance work. The integrated leading edge skin comprises a leading edge structure skin and a plurality of electronic reconnaissance antenna units which are integrally formed, and the electronic reconnaissance antennas are embedded in the leading edge structure skin and are designed along with the shape of the leading edge structure skin. The technical problems that the installation space of an existing electronic reconnaissance antenna is too large, and the stealth performance of the front edge of the position where the electronic reconnaissance antenna is installed is poor are solved.

    本发明提供一种无人机隐身前缘及无人机,无人机隐身前缘包括前缘骨架组件;一体化前缘蒙皮,所述一体化前缘蒙皮沿前缘骨架的长度方向设置在所述前缘骨架上,所述一体化前缘蒙皮用于形成前缘气动外形并且作为电子侦察天线进行侦察工作,所述一体化前缘蒙皮包括一体化成型的前缘结构蒙皮和若干个电子侦察天线单元,所述电子侦察天线预埋在所述前缘结构蒙皮内部并且与前缘结构蒙皮随形设计。本发明解决了现有电子侦察天线安装空间过大且安装电子侦察天线位置前缘隐身性能不好的技术问题。


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    Titel :

    Unmanned aerial vehicle stealth leading edge and unmanned aerial vehicle


    Weitere Titelangaben:

    无人机隐身前缘及无人机


    Beteiligte:
    WEI NANNAN (Autor:in) / YANG XIAOYA (Autor:in) / LI XUAN (Autor:in) / LIU WEI (Autor:in) / ZHOU YONGKANG (Autor:in)

    Erscheinungsdatum :

    26.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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