The invention relates to an aircraft cabin separation covering cap structure which comprises a separation baffle, a covering cap bearing structure and a separation body, the separation baffle is used for sealing a cabin opening, and one end of the separation baffle is used for being connected with a cabin body; the covering cap bearing structure comprises a connecting part and a separating part, the connecting part is arranged at the other end of the separating baffle, and the separating part is connected to the middle of the connecting part; the separating body is connected with the separating part; wherein the connection part and the separation part are configured as follows: when the separation body is separated, the connection part and the separation baffle are fixed on the cabin body, and the separation part and the separation body are separated from the connection part, so that a cavity is formed in the middle of the separation covering cap structure, one end of the cavity is open, and the other end of the cavity is closed by the separation baffle. Before the aircraft carries out covering cap separation work, the separation covering cap structure and the cabin body are connected into a whole through the separation baffle, gap heat between the separation covering cap structure and the cabin body does not need to be treated, after the separation body is separated, the connecting part and the separation baffle are still fixed to the cabin body, the integrity of the structure of the cabin body is guaranteed, and operation of equipment in the cabin is guaranteed.

    本申请涉及一种飞行器舱分离口盖结构,其包括:分离挡板、口盖承载结构和分离体,分离挡板用于封闭舱口,且一端用于与舱体连接;口盖承载结构包括连接部和分离部,连接部设置于分离挡板另一端,分离部连接于连接部中部;分离体与分离部连接;其中,连接部和分离部配置为:当分离体分离时,连接部与分离挡板固定于舱体上,分离部与分离体脱离连接部,以使分离口盖结构中部形成一腔体,腔体一端开口,另一端由分离挡板封闭。本发明在飞行器进行口盖分离工作前,分离口盖结构与舱体通过分离挡板连接成一体,不用处理分离口盖结构与舱体之间的缝隙热,分离体分离后,连接部与分离挡板仍然固定于舱体上,保证舱体的结构的完整性,保障舱内设备的运行。


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    Titel :

    Aircraft cabin separation covering cap structure


    Weitere Titelangaben:

    一种飞行器舱分离口盖结构


    Beteiligte:
    TAN YOUDE (Autor:in) / SHI JIANGBO (Autor:in) / CHEN WEI (Autor:in) / MA XIONGHONG (Autor:in) / SHENG SHILONG (Autor:in) / CHEN XIAOYU (Autor:in) / ZHOU YIMING (Autor:in) / YU MUQI (Autor:in) / GAO YUFEI (Autor:in) / QU ZHENGGANG (Autor:in)

    Erscheinungsdatum :

    10.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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