The invention provides a high temperature resistant wave-transparent wing structure and an aircraft, the high temperature resistant wave-transparent wing structure comprises a wing skeleton, a lower skin, a wingtip structure, an adjusting band plate and an upper skin, the skin can be independently used as the skin, and the skin and an antenna can be integrally formed and then installed on the wing skeleton in a blocking manner. And when the wing skin is independently used as the skin, the antenna is mounted on a spar and a side rib of the wing framework. The high-speed flight platform wingtip structure and the antenna can be integrally formed into a wingtip antenna integrated structure, and the high-speed flight platform wingtip structure and the antenna can also be independently prepared into a wingtip antenna separated structure. A connector, a secondary spar, a wing rib and a bevel edge rib of the wing framework are made of high-temperature-resistant resin-based composite materials, and a main spar, a main wing rib and a rear main spar are made of high-temperature-resistant titanium alloy materials. According to the technical scheme, the technical problems that in the prior art, titanium alloy is adopted as a wing bearing structure material, the wave transmission performance is not achieved, and the early warning detection capacity of a high-speed flight platform is greatly restricted are solved.

    本发明提供了一种耐高温透波机翼结构及飞行器,包括机翼骨架、下蒙皮、翼尖结构、调整带板和上蒙皮,其中蒙皮可以单独作为蒙皮使用,也可与天线一体化成型后,分块安装于机翼骨架上。当机翼蒙皮单独作为蒙皮使用时,天线安装在机翼骨架的翼梁、边肋上。高速飞行平台翼尖结构可以与天线一体化成型为翼尖天线一体化结构,也可与天线各自独立制备形成翼尖天线分开结构。机翼骨架的接头、次翼梁、翼肋和斜边肋采用耐高温树脂基复材,主翼梁、主翼肋和后主翼梁采用耐高温钛合金材料。应用本发明的技术方案,以解决现有技术中采用钛合金作为机翼承载结构材料,不具备透波性能,极大制约了高速飞行平台的预警探测能力的技术问题。


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    Titel :

    High-temperature-resistant wave-transparent wing structure and aircraft


    Weitere Titelangaben:

    耐高温透波机翼结构及飞行器


    Beteiligte:
    GUO WEI (Autor:in) / JIN LIANG (Autor:in) / LIU HAITAO (Autor:in) / CHU XIANYING (Autor:in) / CUI WEI (Autor:in) / GAO ZHENCHAO (Autor:in) / WANG ZHONGSHU (Autor:in) / LIU YANQI (Autor:in) / MA YINWEI (Autor:in) / ZHANG XUDONG (Autor:in)

    Erscheinungsdatum :

    14.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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