The invention belongs to the technical field of aviation, and relates to an aircraft four-side array configuration device. Comprising an in-cabin assembly, an out-cabin assembly and a disc assembly, the in-cabin assembly diffuses an out-cabin load to fuselage skin, a stringer, a floor cross beam and a floor lower frame edge, and force transmission and balance are achieved; the extra-cabin assembly diffuses the load of the upper disc assembly to the fuselage skin, the stringer and the floor cross beam through the extra-cabin assembly, so that force transmission and balance are achieved; the disc assembly diffuses loads to fuselage skins, stringers and floor cross beams through the outboard assembly, and force transmission and balance are achieved.

    本发明属于航空技术领域,涉及一种飞机四面阵构型装置。包括:舱内组合件、舱外组合件以及圆盘组合件,其中,舱内组合件将舱外载荷扩散于机身蒙皮、长桁、地板横梁和地板下框缘,达到力的传递和平衡;舱外组合件将上部圆盘组合件的载荷通过舱外组合件扩散给机身蒙皮、长桁和地板横梁,达到力的传递和平衡;圆盘组合件将载荷通过舱外组合件扩散给机身蒙皮、长桁和地板横梁,达到力的传递和平衡。


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    Title :

    Airplane four-side array configuration device


    Additional title:

    一种飞机四面阵构型装置


    Contributors:
    WU YANPING (author) / FANG JIN (author) / FANG TIANZHENG (author) / ZHAI KAIGE (author) / CHEN HAIJIAN (author)

    Publication date :

    2025-03-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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