The invention discloses a connecting and adjusting structure used at the connecting position of aircraft cabins. The connecting and adjusting structure comprises an H-shaped connecting part and an aircraft cabin component arranged at the connecting end, the connecting end can be embedded into the connecting part, a wedge block cavity is arranged in the middle portion of the connecting part, and a wedge block is arranged in the wedge block cavity; a threaded hole is arranged in the wedge block, the axis of the threaded hole is parallel to the axis of the connecting part, an adjusting bolt is arranged in the middle portion of the connecting part and is matched with the threaded hole arranged on the wedge block, the axis of the adjusting bolt is parallel to the axis of the connecting part, and the wedge block is driven to move in the wedge block cavity in the axis direction of the connecting part when the adjusting bolt rotates; and a wedge-shaped face is arranged on the connecting end, and a wedge-shaped face of the wedge block is attached to the wedge-shaped face of the connecting end. The invention further discloses an adjusting method, effective adjustment on the connected aircraft cabins is achieved, and bosses and the like appearing in the connecting positions of adjacent aircraft cabins are avoided.


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    Titel :

    Connecting and adjusting structure for aircraft cabins and adjusting method


    Beteiligte:

    Erscheinungsdatum :

    21.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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