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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    CIRCUMFERENTIAL LAP SPLICES FOR SECTIONS OF FUSELAGE


    Beteiligte:
    MACKO PATRICK J (Autor:in) / AUTRY BYRON JAMES (Autor:in) / KENDALL JAMES R (Autor:in) / KNUTSON SAMUEL JAMES (Autor:in) / PETERS BRIAN T (Autor:in) / BAILEY MICHAEL J (Autor:in) / STAUFFER MATTHEW S (Autor:in) / WANTHAL STEVEN (Autor:in) / MEJIA SANTIAGO M (Autor:in) / MURPHY SARA (Autor:in)

    Erscheinungsdatum :

    23.06.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



    CIRCUMFERENTIAL LAP SPLICES FOR SECTIONS OF FUSELAGE

    MACKO PATRICK J / AUTRY BYRON JAMES / KENDALL JAMES R et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Circumferential lap splices for sections of fuselage

    MACKO PATRICK J / AUTRY BYRON JAMES / KENDALL JAMES R et al. | Europäisches Patentamt | 2024

    Freier Zugriff