The invention discloses an aircraft wing lightning protection skin structure, specifically, a skin layer is sequentially covered with a resin adhesive layer, a conductive copper mesh layer and a protective coating, a conductive mesh can effectively capture and disperse lightning current and can also be tightly connected with a metal structure in a wing, and direct damage of lightning to the interior of an aircraft is avoided. The resin adhesive layer contains the conductive filler, so that the lightning current dispersing capability of the skin is further improved, the lightning protection capability of the aircraft wing is improved, and the safety performance and the reliability of the aircraft are improved.

    本发明公开了一种飞机机翼防雷击的蒙皮结构,具体为在蒙皮层依次覆盖树脂胶层、导电铜网层和保护涂层,导电网格不仅能够有效捕捉和分散雷电电流,还能与机翼内部的金属结构紧密相连,避免雷电对飞机内部的直接损害。树脂胶层含有导电填料,进一步提高了蒙皮的分散雷电电流的能力,提高飞机机翼的防雷击能力,从而提高飞机的安全性能和可靠性。


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    Titel :

    Lightning protection skin structure of aircraft wing


    Weitere Titelangaben:

    一种飞机机翼防雷击的蒙皮结构


    Beteiligte:
    TANG SHAOCHUN (Autor:in) / HAN JINGCHUANG (Autor:in)

    Erscheinungsdatum :

    03.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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