An aircraft pressurized cabin door includes an integral door structure unit made of fiber composite, the unit including an outer skin and a door framework arranged on an inner side of the outer skin. The framework includes a plurality of edge supports and a plurality of longitudinal supports extending in a width direction between the edge supports so as to form door framework interstices delimited by the inner side of the outer skin, by the edge supports and by the longitudinal supports. The door framework interstices are configured in a manner open toward the inner side of the door.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft pressurized cabin door made of fiber composite


    Contributors:

    Publication date :

    2015-10-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT PRESSURIZED CABIN DOOR WITH A STRUCTURE FORMED BY BEAMS

    DEVILLEZ SABASTIEN | European Patent Office | 2021

    Free access

    Notes on design of pressurized cabin aircraft

    Dommasch, D.O. | Engineering Index Backfile | 1946


    Aircraft mission cabin door structure

    YU SHAOYANG / LIU WANCHUN / WANG BAOFENG et al. | European Patent Office | 2024

    Free access

    Aircraft cabin door lifting device

    YAN DONGFENG / YE LU / CHEN XI et al. | European Patent Office | 2023

    Free access

    Aircraft cabin section, door insulation and aircraft

    KIRSTEIN HENNING / KYAS GYORGY | European Patent Office | 2022

    Free access