According to a method for eliminating the assembly gap between an airplane transition beam and a hanging frame, a groove-shaped double-lug connecting hole is formed in the hanging frame, a single-lug connecting hole is formed in the airplane transition beam and is coaxial with the groove-shaped double-lug connecting hole of the hanging frame, a shouldered lining in clearance fit is arranged in a hole in one side of the groove-shaped double-lug connecting hole of the hanging frame, the shoulder part of the shouldered lining is positioned on the inner side of the hole, and the length of the shouldered lining is greater than the thickness of the groove-shaped double-lug lug of the hanging frame; the groove-shaped double-lug connecting hole of the hanging frame is connected with the single-lug connecting hole of the transition beam through a bolt and a nut, and the assembly gap between the airplane transition beam and the hanging frame is eliminated by tightening the nut and pressing the shouldered lining.

    一种消除飞机过渡梁与挂架装配间隙的方法,挂架上设有槽型双耳连接孔,飞机过渡梁上有单耳连接孔,该单耳连接孔与挂架槽型双耳连接孔同轴,在挂架槽型双耳连接孔的一侧孔内设有间隙配合的带肩衬套,该带肩衬套的肩部位于孔的内侧,带肩衬套的长度大于挂架槽型双耳耳片的厚度;通过螺栓螺母将挂架槽型双耳连接孔与过渡梁的单耳连接孔连接,通过拧紧螺母压紧带肩衬套消除飞机过渡梁与挂架装配间隙。


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    Titel :

    Method for eliminating assembly gap between airplane transition beam and hanging frame


    Weitere Titelangaben:

    一种消除飞机过渡梁与挂架装配间隙的方法


    Beteiligte:
    WU PINGJUN (Autor:in) / LI XINGFU (Autor:in) / QU CHUNYUAN (Autor:in)

    Erscheinungsdatum :

    07.09.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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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