The invention discloses a carbon fiber composite aircraft cabin shell and an assembling method thereof.The carbon fiber composite aircraft cabin shell comprises a cabin main shell and a shelf in the shape of a Chinese character'yue ', and the shelf in the shape of the Chinese character'yue' is detachably connected to the interior of the cabin main shell; a front bearing part and a rear bearing part are arranged at the two ends of the cabin section main shell correspondingly, the side, close to the front bearing part, of the cabin section main shell is of an open structure, bearing part assembling holes are evenly distributed in the front bearing part and the rear bearing part in the circumferential direction, a rectangular pit is formed in the top of the cabin section main shell, and long-strip-shaped pits are symmetrically formed in the bottom of the cabin section main shell. Assembly holes are formed in the two sides of the cabin section main shell, and embedded nut holes corresponding to the assembly holes are formed in the two side walls of the shelf shaped like the Chinese character'yue '. The cabin shell is light in weight, high in strength, stable in structure and capable of being rapidly connected with and detached from an unmanned aerial vehicle and a warhead section, signal receiving is free of interference, and the module units are integrated, installed, disassembled and assembled conveniently.

    本发明公开了一种碳纤维复合材料航空器舱段壳体及其组装方法,包括舱段主壳体和曰形层架,所述曰形层架可拆卸连接在舱段主壳体的内部;舱段主壳体的两端分别设置前承接部和后承接部,且舱段主壳体靠近前承接部的一侧为敞口结构,前承接部和后承接部均周向均布有承接部装配孔,舱段主壳体的顶部设有长方形凹陷,舱段主壳体的底部对称设有长条形凹陷,所述舱段主壳体的两侧设有装配孔,所述曰形层架的两侧壁设置有与装配孔相对应的预埋螺母孔。本发明提供一种轻质高强、结构稳固、与无人机和战斗部段可快速连接与拆卸的舱段壳体,并实现信号接收无干扰,模块单元集成安装与拆装便捷。


    Access

    Download


    Export, share and cite



    Title :

    Carbon fiber composite aircraft cabin shell and assembling method thereof


    Additional title:

    一种碳纤维复合材料航空器舱段壳体及其组装方法


    Contributors:
    LI YI (author) / WEI XIUBIN (author)

    Publication date :

    2023-12-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



    DISPLAY DEVICE, AIRCRAFT CABIN AND METHOD FOR ASSEMBLING AN AIRCRAFT CABIN

    JAFFRELOT JEAN-BAPTISTE | European Patent Office | 2024

    Free access

    DISPLAY DEVICE, AIRCRAFT CABIN AND METHOD FOR ASSEMBLING AN AIRCRAFT CABIN

    JAFFRELOT JEAN-BAPTISTE | European Patent Office | 2024

    Free access

    Aircraft pressurized cabin door made of fiber composite

    HAENSCH PETER / MUELLER REINHARD / BRAUN RICHARD et al. | European Patent Office | 2015

    Free access

    Split type modular cabin and assembling method thereof

    ZHANG XINGHONG / KANG JIE / LEE JUNG KYU | European Patent Office | 2022

    Free access

    CABIN FLOOR FOR AN ELEVATOR CABIN AND METHOD FOR ASSEMBLING AN ELEVATOR CABIN

    LO JACONO ROMEO / CARRARA ELENA / STEINER KURT et al. | European Patent Office | 2025

    Free access