A jig apparatus and associated systems and methods for forming a composite wing skin is presented, including providing a frame with a working surface. A plurality of indexing blocks are coupled to the working surface of the frame. Each of the plurality of indexing blocks has a first indexing surface oriented perpendicular to the working surface of the frame and a second indexing surface oriented approximately parallel to the working surface of the frame. A plurality of clamping blocks are also each moveably coupled to one of the plurality of indexing blocks. Each of the plurality of clamping blocks has a clamping surface oriented perpendicular to the working surface of the frame and in facing relation to the first indexing surface of an adjacent indexing block thereby defining a plurality of channels.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Method, System and Apparatus for Assembling a Composite Wing Skin with Stiffeners


    Beteiligte:

    Erscheinungsdatum :

    2016-08-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    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



    METHOD, SYSTEM AND APPARATUS FOR ASSEMBLING COMPOSITE WING SKIN WITH STIFFENERS

    DOAN DINH PHAM / MARK CHARLES IDEN | Europäisches Patentamt | 2016

    Freier Zugriff

    Method, system and apparatus for assembling a composite wing skin with stiffeners

    PHAM DOAN DINH / IDEN MARK CHARLES | Europäisches Patentamt | 2018

    Freier Zugriff

    Mandrel forming for discrete wing skin stiffeners

    HUDDLESTON NICHOLAS LEE / BALLESTER JAIME | Europäisches Patentamt | 2020

    Freier Zugriff

    Mandrel Forming for Discrete Wing Skin Stiffeners

    HUDDLESTON NICHOLAS LEE / BALLESTER JAIME | Europäisches Patentamt | 2016

    Freier Zugriff

    Mandrel forming for discrete wing skin stiffeners

    HUDDLESTON NICHOLAS LEE / BALLESTER JAIME | Europäisches Patentamt | 2017

    Freier Zugriff