To provide systems and methods for inspecting a wing panel.SOLUTION: Methods include advancing a wing panel through a Non-Destructive Inspection (NDI) station, and inspecting the wing panel with inspection heads at the NDI station. The wing panel may be suspended beneath a strongback during the inspection, e.g., by using vacuum couplers and/or adjustable-length pogos of the strongback, and the suspending may include enforcing a contour to the wing panel using the vacuum couplers and/or pogos. Other methods include receiving a wing panel at an NDI station, and inspecting a portion of the wing panel during movement through the NDI station.SELECTED DRAWING: Figure 7

    【課題】翼パネルを検査するためのシステム及び方法が提供される。【解決手段】非破壊検査(NDI)ステーションを通して、翼パネルを前進させることと、NDIステーションにおいて、検査ヘッドを用いて、翼パネルを検査することとを含む。翼パネルは、例えば、ストロングバックの真空連結器及び/又は長さ調整可能なポゴを使用して、検査の間にストロングバックの下に吊り下げられてもよく、吊り下げることは、真空連結器及び/又はポゴを使用して、輪郭を翼パネルに生じさせることを含み得る。他の方法は、NDIステーションにおいて翼パネルを受け入れることと、NDIステーションを通して動いている間、翼パネルの一部を検査することとを含む。【選択図】図7


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    Title :

    ASSEMBLY LINE FABRICATION AND ASSEMBLY OF AIRCRAFT WINGS


    Additional title:

    組み立てライン製造及び航空機の翼の組み立て


    Contributors:

    Publication date :

    2022-05-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    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 / B64C AEROPLANES , Flugzeuge



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