The invention belongs to the technical field of technological equipment design and manufacturing, and relates to an aircraft panel butt joint positioning detection method. Specifically, the device is used for detecting the positions of all stringers after aircraft panels are butted and assembled, and is used for detecting the positions of the stringers and skins at the butted positions after the panels are assembled and butted. The method solves the problem that positioning positions of a stringer, a base plate and the like at the butt joint position after wall plates are in butt joint are lack of special inspection means, and the method does not affect use of an assembly fixture and does not affect the assembly progress during detection. The detection device is simple in design, low in manufacturing cost and small in occupied area.

    本发明属于工艺装备设计及制造技术领域,涉及一种飞机壁板对接定位检测方法。具体地说,是关于飞机壁板对接装配完成后对所有长桁位置,用于壁板装配对接完成后对对接位置的长桁和蒙皮位置进行检测。解决了壁板对接后对接处的长桁,垫板等定位位置缺乏专用检验手段的问题,该方法检测时不会影响装配型架的使用,不会影响装配进度。检测装置设计简单,制造成本低,占地面积小。


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    Title :

    Airplane panel butt joint positioning detection method


    Additional title:

    一种飞机壁板对接定位检测方法


    Contributors:
    JIN ZHAO (author) / LIU JIANCHAO (author) / ZHANG JIA (author) / YU ZHILIANG (author) / DONG LU (author) / ZHANG HAORAN (author) / GU TIANYU (author) / DAI FAN (author)

    Publication date :

    2024-01-09


    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



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