The invention discloses an aircraft with wing and cabin section heat insulation structures, and relates to the technical field of high-speed aircraft heat protection, the aircraft comprises a cabin section, and a cabin section mounting hole is formed in the cabin section; wings, wherein wing joint devices are arranged on the wing, and the wings are mounted on the cabin section through the wing joint devices; and a thermal protection assembly which comprises a cabin thermal protection assembly arranged between the end face of the wing joint device and the mounting hole, and a wing thermal protection assembly arranged between the side face of the wing joint device and the side wall of the mounting hole. According to the aircraft, the applicant arranges the heat-proof structure which completely covers the connecting part of the wing and the cabin section at the connecting part of the wing and the cabin section, so that the heat transfer efficiency of the high-temperature wing is effectively reduced, and a system in the cabin section of the aircraft cannot normally operate due to heat transfer of the wing.

    本发明公开了一种具有机翼与舱段绝热结构的飞行器,涉及高速飞行器热防护技术领域,该装置包括舱段,所述舱段上设有舱段安装孔;机翼,所述机翼上设有机翼接头装置,所述机翼通过所述机翼接头装置安装于所述舱段;热防护组件,其包括设于所述机翼接头装置的端面与所述安装孔之间的舱段热防护组件,以及设于所述机翼接头装置侧面与所述安装孔侧壁之间的机翼热防护组件。本方案中申请人通过在机翼与舱段的连接部分设置全面覆盖机翼与舱段的连接部分的防热结构,有效降低了高温的机翼的热量传递效率,使飞行器舱段内的系统不会因机翼的热传递而无法正常运转。


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    Titel :

    Aircraft with wing and cabin section heat insulation structure


    Weitere Titelangaben:

    一种具有机翼与舱段绝热结构的飞行器


    Beteiligte:
    WANG QIAOYUN (Autor:in) / ZOU TIANPING (Autor:in) / HU SHANGANG (Autor:in) / LIU QING (Autor:in) / WANG BOZHE (Autor:in) / TAN YOUDE (Autor:in) / HU CHI (Autor:in)

    Erscheinungsdatum :

    2022-01-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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