An internal fixed structure for a nacelle, comprising end panels, an intermediate panel in the form of a half-cylinder between the end panels, splice plates between the intermediate panel and each end panel, wherein each splice plate is made up of a skin with an inner face fastened to the panels and at least one indentation protruding with respect to an outer face, and a pad fastened to each fastening surface of an indentation, wherein each pad of the upper splice plate bears against a surface of an engine pylon, and wherein each pad of the lower splice plate bears against a pad of a lower splice plate of another internal fixed structure.


    Access

    Download


    Export, share and cite



    Title :

    INTERNAL FIXED STRUCTURE FOR AN AIRCRAFT NACELLE


    Contributors:

    Publication date :

    2024-10-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    AIRCRAFT NACELLE INTERNAL STRUCTURE

    HURLIN HERVE / KERBLER OLIVIER / GILO OLIVIER | European Patent Office | 2015

    Free access

    Aircraft nacelle section and aircraft having aircraft nacelle section

    WEN AMY / KIRSTEIN HENNING / TEICHMANN SIEGFRIED et al. | European Patent Office | 2022

    Free access

    AIRCRAFT NACELLE

    DELSOL DAVID / KERKABOU SABRINA / KHEZZAR ALI | European Patent Office | 2020

    Free access

    Nacelle and aircraft equipped with nacelle

    LIU KAILI / WANG LEI / SHAO QINGLING et al. | European Patent Office | 2021

    Free access

    Aircraft nacelle noise elimination structure

    LIU QIAN / MA LIMIN / HU ZHENDONG et al. | European Patent Office | 2021

    Free access