The invention relates to composite material skin net edge coordination tools and an assembling method for skins. The method comprises following steps: 1) arranging coordinators on the skin assembling tools, wherein the coordinators are provided with coordination holes; 2) mounting the skins on corresponding assembling racks, and prepositioning and clamping the skins; 3) drilling technologic holes in the skins through the coordination holes in the net edge coordinators; 4) positioning and fixing the skins on the corresponding racks through the coordination holes in the skins; 5) drawing net edge lines on the surfaces of the skins by the use of line drawing templates; 6) performing trimming based on the net edge lines after the skins are disassembled; and 7) assembling and positioning the different skins on an assembly frame through butt joint coordination holes. According to the invention, the net edge size of the skins are determined through the cooperation of the net edge coordinators and the line drawing templates, and the skins are positioned through the butt joint coordination holes in an assembling process, so that the accuracy of the net edge size of the composite material skins is improved, the structure of the frame is simplified, the operation is easy and visual, and the assembling efficiency is improved.


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    Titel :

    Composite material skin net edge coordination tools and assembling method for skins


    Beteiligte:
    WANG XIN (Autor:in) / ZHANG YI (Autor:in) / WANG SHAOQIANG (Autor:in) / ZHANG PENG (Autor:in) / WANG AICHUN (Autor:in) / LIU HONGTAO (Autor:in) / WANG XINXING (Autor:in)

    Erscheinungsdatum :

    2015-11-11


    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



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