The invention relates to an aircraft window consisting of an inner panel (1) and an outer panel (2) which are separated by a layer of air (3) and by an installation seal (4) into which a peripheral portion of the window is set, the inner panel (1) consisting of a first, outer pane of glass (11) and a second, inner pane of glass (12), each having a thickness from 0.1 mm to 3 mm and being bonded to one another by a first adhesive interlayer (13) with a thickness from 50 µm to 2 mm, and/or the outer panel (2) consisting of a first, outer sheet of transparent structural polymer material (21) with a thickness from 1.5 mm to 100 mm bonded to a third, inner pane of glass (22) with a thickness from 0.1 mm to 30 mm by means of a second adhesive interlayer (23) with a thickness from 50 µm to 2 mm.


    Access

    Download


    Export, share and cite



    Title :

    HUBLOT D'AERONEF ALLEGE A RIGIDITE EGALE


    Additional title:

    AIRCRAFT WINDOW WITH REDUCED WEIGHT BUT THE SAME RIGIDITY
    FLUGZEUGFENSTER MIT REDUZIERTEM GEWICHT ABER GLEICHER STEIFIGKEIT


    Contributors:

    Publication date :

    2024-08-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Hublot d’aéronef allégé à rigidité égale

    ROUBY MICHEL / DUFFOUR ADRIEN | European Patent Office | 2024

    Free access

    HUBLOT D'AERONEF ALLEGE A RIGIDITE EGALE

    ROUBY MICHEL / DUFFOUR ADRIEN | European Patent Office | 2023

    Free access

    HUBLOT D'AVION ALLEGE A FAIBLE TRAÎNEE

    ROUBY MICHEL / SAUVESTY JEAN-CHARLES / SIMON SÉBASTIEN | European Patent Office | 2022

    Free access