The invention relates to a method and structural gap filler for optimized assembly. Drill cuttings generated between the first component and the second component during drilling of the injection hole are encapsulated by injecting a structural gap filler between the first component and the second component via the injection hole.

    本发明上涉及用于优化组装的方法和结构间隙填料。通过经由注入孔在第一部件与第二部件之间注入结构间隙填料来封装在注入孔的钻设期间在第一部件和第二部件之间生成的钻屑。


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    Title :

    Method and structural gap filler for optimized assembly


    Additional title:

    用于优化组装的方法和结构间隙填料


    Contributors:

    Publication date :

    2024-04-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B26D Schneiden , CUTTING / 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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