A joint for connecting a central wing box and a bay of an aircraft. The joint includes a bend corner member having a first portion shaped to abut against and connect to the central wing box, a second portion shaped to abut against and connect to a first side of a deck of the bay, and an intermediate rounded corner portion located between the first portion and the second portion. A first support member is attached to the central wing box at a first pin and supports a first side of a second portion of the bend corner member. A second support member is attached to the web of the bay at a second pin and supports a second side of the second portion of the bend angle member. A first support member is positioned on a first side of a deck of the bay, and a second support member is positioned on an opposing second side of the deck.

    一种飞机的用于连接中央翼盒和隔舱的接头。接头包括弯曲角构件,该弯曲角构件具有被成形为邻接抵靠并连接到中央翼盒的第一部分,被成形为邻接抵靠并连接到隔舱的甲板的第一侧的第二部分,以及位于第一部分和第二部分之间的中间圆形拐角部。第一支撑构件在第一销处附接到中央翼盒并支撑弯曲角构件的第二部分的第一侧。第二支撑构件在第二销处附接到隔舱的腹板并支撑弯曲角构件的第二部分的第二侧。第一支撑构件定位在隔舱的甲板的第一侧上,并且第二支撑构件定位在甲板的背对的第二侧上。


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    Title :

    Joint for connecting central wing box and compartment in aircraft


    Additional title:

    在飞机中用于连接中央翼盒和隔舱的接头



    Publication date :

    2022-07-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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