The invention relates to a novel missile body cabin section connecting mechanism which comprises a first wedge-shaped block, a second wedge-shaped block, a front cabin and a rear cabin, the front cabin and the rear cabin are each of a cylindrical structure, the front cabin comprises a front cabin large-diameter section and a front cabin small-diameter section, and the front cabin small-diameter section is in butt joint with the rear cabin small-diameter section; trapezoidal teeth are uniformly distributed on the small-diameter section of the front cabin along the radial direction of the circumference; a circumferential inclined surface is processed at the joint of the forecabin large-diameter section and the forecabin small-diameter section, and is as high as the ring teeth; a positioning groove is formed in the top of the joint of the forecabin large-diameter section and the forecabin small-diameter section; the rear cabin comprises a rear cabin large-diameter section and a rear cabin small-diameter section; trapezoidal teeth are uniformly distributed on the small-diameter section of the rear cabin in the circumferential radial direction; a rectangular groove is formed between two trapezoidal teeth of the large-diameter section of the rear cabin and is used for mounting a first wedge-shaped block and a second wedge-shaped block; trapezoidal teeth are machined on the front cabin small-diameter section and the rear cabin small-diameter section, and it is guaranteed that the rear cabin trapezoidal teeth can pass through the space between the front cabin trapezoidal teeth. The waterproof performance and the bearing capacity of the product are effectively improved.

    本发明涉及一种新型弹体舱段连接机构,包括:第一楔形块、第二楔形块、前舱和后舱,前舱与后舱均为圆筒状结构,前舱包括前舱大径段和前舱小径段,前舱小径段与后舱小径段对接;前舱小径段沿着圆周径向方向均匀分布梯形齿;前舱大径段和前舱小径段连接处加工圆周斜面,高度与环齿高度一致;前舱大径段和前舱小径段连接处顶部开有定位槽;后舱包括后舱大径段和后舱小径段;后舱小径段沿着圆周径向方向均匀分布梯形齿;后舱大径段在两个梯形齿中间加工矩形槽,用于安装第一楔形块和第二楔形块;前舱小径段和后舱小径段加工有梯形齿,保证后舱梯形齿能通过前舱梯形齿间的空间。本发明有效提升防水性能以及产品的承载能力。


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    Titel :

    Novel missile body cabin section connecting mechanism


    Weitere Titelangaben:

    一种新型弹体舱段连接机构


    Beteiligte:
    ZHANG HUAFENG (Autor:in) / GAO XIUHUA (Autor:in) / MENG FEI (Autor:in) / YUE ZHENG (Autor:in) / WANG ZHIWEI (Autor:in) / SHI BOWEI (Autor:in) / TANG YIHONG (Autor:in)

    Erscheinungsdatum :

    2023-01-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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