Systems and methods for assembling aircraft fuselages are provided, in particular frame mounting stations for segments of aircraft fuselages. An embodiment is a method for assembling an aircraft fuselage. The method includes indexing an arcuate section of the fuselage to a frame mounting station, feeding a frame into a recess defined by the arcuate section at the frame mounting station, placing the frame against an inner mold line (IML) of the arcuate section while the frame is within the recess, and securing the frame to the arcuate section.

    提供了用于组装飞行器机身的系统和方法,尤其是提供了用于飞行器机身段的框架安装工位。实施方式是一种用于组装飞行器机身的方法。该方法包括将机身的弓形区段转位到框架安装工位,在框架安装工位将框架进给到由弓形区段限定的凹部中,当框架在凹部内时将框架抵靠弓形区段的内模线(IML)放置,以及将框架固定到弓形区段。


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    Title :

    Frame mounting station for aircraft fuselage section


    Additional title:

    用于飞行器机身段的框架安装工位


    Contributors:

    Publication date :

    2022-05-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    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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