The invention relates to a fastening system for an aircraft structure. The fastening system that couples a first aircraft structure and a second aircraft structure is disclosed. The fastening system includes a fastener, a nut plate having a main body defining an opening to receive the fastener, a flange extending from the main body to engage an outer surface of the first structure, and a first sleeve protruding from the flange in a direction away from the main body, and the first sleeve is coupled to a first bore formed in the first structure and prevents the rotation of the nut plate relative to the first structure.

    本发明涉及用于飞机结构的紧固系统。公开了一种耦接第一飞机结构和第二飞机结构的紧固系统。所述紧固系统包括紧固件、螺母板、凸缘和第一套筒,所述螺母板具有限定开口以接收所述紧固件的主体,所述凸缘从所述主体延伸以接合所述第一结构的外表面,所述第一套筒在远离所述主体的方向上从所述凸缘突出,所述第一套筒耦接到形成在所述第一结构中的第一镗孔,并且防止所述螺母板相对于所述第一结构的旋转。


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    Title :

    Fastening system for aircraft structure


    Additional title:

    用于飞机结构的紧固系统


    Contributors:

    Publication date :

    2022-01-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile / B64C AEROPLANES , Flugzeuge



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