Systems and methods are provided for splicing airframe components. One embodiment is a method for assembling an airframe of an aircraft. The method includes forming a first skin of a first circumferential section of fuselage, the first skin including a distal portion comprising a lip and a shoulder, aligning a second skin of a second circumferential section of fuselage with the shoulder such that the lip overlaps the second skin, and affixing the first skin and the second skin together via a circumferential splice.


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    Title :

    CIRCUMFERENTIAL LAP SPLICES FOR SECTIONS OF FUSELAGE


    Additional title:

    UMFANGSVERBINDUNGEN FÜR RUMPFSEKTIONEN
    RACCORDS CIRCONFÉRENTIELS POUR DES SECTIONS DE FUSELAGE



    Publication date :

    2022-06-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Circumferential lap splices for sections of fuselage

    MACKO PATRICK J / AUTRY BYRON JAMES / KENDALL JAMES R et al. | European Patent Office | 2024

    Free access

    CIRCUMFERENTIAL LAP SPLICES FOR SECTIONS OF FUSELAGE

    MACKO PATRICK J / AUTRY BYRON JAMES / KENDALL JAMES R et al. | European Patent Office | 2022

    Free access