PROBLEM TO BE SOLVED: To provide a system and a method for reinforcing contours onto parts of an aircraft.SOLUTION: A reinforced brace 700 is provided, and a contour is reinforced onto a panel of a barrel section. The panels 410-440 are arranged in a manner that a plurality of outer plate lap joints 1000 can complete together to form the barrel section 132. For example, a contour defined for the panel 410 can be temporarily reinforced by the brace 700 so that the panel is reliably and properly integrated with the other panel. The brace 700 can be removed after playing the temporary role.SELECTED DRAWING: Figure 13

    【課題】航空機部品の方に向かって輪郭を強化するためのシステム及び方法を提供する。【解決手段】強化されたブレース700が提供され、バレル部分のパネルの方に向かって輪郭が強化される。パネル410−440は、複数の外板の重ね継ぎ1000が、バレル部分132を形成するためにまとめて完成し得るように配置される。例えばパネル410用に画定される輪郭は、パネルが他のパネルと確実に正しく統合されるように、ブレース700によって一時的に強化され得る。ブレース700は、その一時的な役割を果たした後に除去され得る。【選択図】図13


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    Title :

    CONTOUR RETENTION IN SEGMENTED FUSELAGE ASSEMBLY


    Additional title:

    分割された胴体アセンブリにおける輪郭保持


    Contributors:

    Publication date :

    2018-02-15


    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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