A system configured for installing or removing a door (104) from an aircraft, comprises: a pin (108), a hinge (202) comprising a slot (208) that forms a cavity for rotatively coupling the hinge (202) and the pin (108), a clamp (210) coupled to the pin (108), and a retaining mechanism (216) on the clamp (210) that selectively bears against the hinge (202) to maintain the pin (108) in the cavity when the retaining mechanism (216) is engaged and releases the hinge (202) when the retaining mechanism (216) is disengaged.


    Access

    Download


    Export, share and cite



    Title :

    HINGE STRUCTURE


    Additional title:

    SCHARNIERSTRUKTUR
    STRUCTURE DE CHARNIERE


    Contributors:

    Publication date :

    2020-09-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E05D Scharniere oder andere Aufhängevorrichtungen für Türen, Fenster oder Flügel , HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS, OR WINGS



    Hinge structure

    European Patent Office | 2019

    Free access

    HINGE STRUCTURE

    DE GRAFF THEO / THOOLEN JOS | European Patent Office | 2022

    Free access

    HINGE STRUCTURE

    NISHIYAMA YUJI / MAYUMI REN | European Patent Office | 2021

    Free access

    Hinge structure

    DE GRAAFF THEO / THOOLEN JOS | European Patent Office | 2024

    Free access

    Hinge structure

    THEO DE GRAAF / JOS THOOLEN | European Patent Office | 2021

    Free access