The invention discloses a wing fuel tank protective cap and a forming process thereof and relates to the technical field of transportation. The wing fuel tank protective cap comprises a cap body; the cap body and a clamping pressure ring clamp skin; the cap body comprises a protective layer and a reinforcement layer inside the protective layer; the protective layer is used for preventing lightning and fire; the reinforcement layer is made of polyethylene fibers and used for achieving the function of resisting outer object impact. According to the forming process of the wing fuel tank protective cap, the wing fuel tank protective cap is formed through a resin transfer molding forming process by preparing corresponding materials. According to the wing fuel tank protective cap and the forming process thereof, the problems in the prior art that a wing fuel tank cap is complex in structure, poor in shock resistance, seriously affected by environmental factors, low in production efficiency and high in cost can be solved.


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    Title :

    Wing fuel tank protective cap and forming process thereof


    Contributors:
    SUN JIANZHUO (author) / ZHAO QUN (author) / XIN CHAOBO (author) / GAO JUBIN (author) / LI XING (author) / LIU CHUANJUN (author)

    Publication date :

    2015-12-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS



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