To provide a joint in fasteners for joining an aircraft wing to an aircraft body, where the joint allows easy access to fastener holes in deburring the fastener holes after drilling.SOLUTION: A joint 18 joining an aircraft wing 14 to an aircraft body employs a splice panel 64 that is engaged in surface engagement with a skin panel 22 on a side of the aircraft body and is engaged in surface engagement with a leg panel 24 extending upwardly from the aircraft wing. Multiple fasteners 76, 82 extend through the splice panel and the leg panel, and extend through the splice panel and the skin panel. The fasteners attach the splice panel to the skin panel and attach the splice panel to the leg panel, thereby attaching the skin panel to the leg panel. After fastener holes have been drilled through the splice panel and the leg panel to attach the splice panel to the leg panel, the splice panel can be removed from the leg panel. This allows easy access to the fastener holes.SELECTED DRAWING: Figure 2

    【課題】航空機の翼を航空機本体に接合するファスナにおいて、ファスナ穴を穿孔後にバリ取りを行う際、ファスナ穴に容易にアクセスする接合部を提供する。【解決手段】航空機の翼14を航空機本体に接合する接合部18に、航空機本体の側面の外板パネル22に面係合状態で係合するとともに航空機翼から上方に延びる脚パネル24に面係合状態で係合する継ぎ目パネル64を用いる。複数のファスナ76、82が、継ぎ目パネル及び脚パネルを貫通するとともに、継ぎ目パネル及び外板パネルを貫通する。前記複数のファスナが、継ぎ目パネルを外板パネルに取り付けるとともに継ぎ目パネルを脚パネルに取り付け、これにより外板パネルを脚パネルに取り付ける。継ぎ目パネルを脚パネルに取り付けるために継ぎ目パネル及び脚パネルにファスナ穴を穿孔した後に、継ぎ目パネルを脚パネルから取り外すことができ、ファスナ穴に容易にアクセスすることができる。【選択図】図2


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    Title :

    JOINT JOINING AIRCRAFT WING TO AIRCRAFT BODY


    Additional title:

    航空機の翼を航空機本体に接合する接合部


    Contributors:

    Publication date :

    2021-07-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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