According to the multifunctional rudder wing structure, a rudder wing is composed of an inner core, an outer layer and an interlayer, and multiple functions such as light weight, high temperature resistance, oil storage and high bearing capacity can be achieved. The rudder wing structure is composed of a closed inner core, a heat preservation and insulation interlayer, a heat insulation column and a high-temperature-resistant outer layer skin. The whole structure comprises a framework, a skin and a heat insulation column. The whole rudder wing not only has better rigidity and strength, but also can solve the problem of heat transfer between the inner layer and the outer layer, meet the low-temperature requirement of internal oil storage, and effectively reduce the weight of the whole structure.

    本发明公开了一种多功能舵翼结构,其中,舵翼由内芯、外层及夹层组成,可以实现轻量化、耐高温、贮油、高承载等多种功能。本发明的舵翼结构由一个封闭内芯、保温隔热夹层、隔热柱和耐高温外层蒙皮四种组元特征构成;整体结构形式为骨架、蒙皮及隔热柱。整个舵翼不仅具有较好的刚度和强度,还可以解决内外层的热传输,满足内部贮油低温需求,有效降低整体结构的重量。


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    Titel :

    Multifunctional rudder wing structure


    Weitere Titelangaben:

    一种多功能舵翼结构


    Beteiligte:
    LI JIANWEI (Autor:in) / LI BAOYONG (Autor:in) / HAN WEIQUN (Autor:in) / GUO XIAOLIN (Autor:in) / LIU JICHEN (Autor:in) / LI XIN (Autor:in) / HAN BING (Autor:in) / QIN ZHONGHUAN (Autor:in) / LIU WEI (Autor:in) / WANG SHENGLONG (Autor:in)

    Erscheinungsdatum :

    2024-01-16


    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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