A method and apparatus for an aircraft structure. In one advantageous embodiment, the aircraft structure (400,526) may have a rib (506-510), a plurality of stringers (512-522), and a set of shear ties (600,602). The plurality of stringers may have skin flanges (608-612) at ends of the plurality of stringers capable of being fastened to skin (524) for the aircraft structure. The set of shear ties may extend from the rib and have a set of elongate members (624-635) in which the set of elongate members are attached to the plurality of stringers.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rib support for wing panels


    Weitere Titelangaben:

    Stützrippen für Flügelpaneele
    Support nervuré pour panneaux ailés


    Beteiligte:
    TANNER RICHARD B (Autor:in) / BURFORD IAN C (Autor:in) / GENDZWILL THOMAS V (Autor:in) / DOTY GREGORY B (Autor:in) / HUCK JAMES R (Autor:in) / WILSON DEAN E (Autor:in) / KORENAGA BRIAN H (Autor:in)

    Erscheinungsdatum :

    02.11.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    WING ASSEMBLY HAVING DISCRETELY STIFFENED COMPOSITE WING PANELS

    BEHZADPOUR FOROUZAN / LEVINE DANIEL M | Europäisches Patentamt | 2022

    Freier Zugriff

    Wing assembly having discretely stiffened composite wing panels

    BEHZADPOUR FOROUZAN / LEVINE DANIEL M | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT WING WITH INTEGRATED SOLAR PANELS

    TYTSYK YURIJ ALEKSANDROVICH / SHPILEVSKIJ VYACHESLAV LEONIDOVICH | Europäisches Patentamt | 2019

    Freier Zugriff

    Contour Assessment of Formed Wing Panels

    Cook, Harold R. | SAE Technical Papers | 1985


    Composite wing panels and fabrication method

    SMITH DANIEL R / JONES DARRELL DARWIN | Europäisches Patentamt | 2024

    Freier Zugriff