A joint joining an aircraft wing to an aircraft body employs a splice panel that is engaged in surface engagement with a skin panel on a side of the aircraft body and is engaged in surface engagement with a leg panel extending upwardly from the aircraft wing. A plurality of fasteners extend through the splice panel and the leg panel and extend through the splice panel and the skin panel. The plurality of fasteners attach the splice panel to the skin panel and attach the splice panel to the leg panel and thereby attach 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 provides easy access to the fastener holes drilled through the leg panel for deburring of the fastener holes.
本公开涉及将飞机机翼连接到飞机主体的接头,该接头采用接头面板,该接头面板与飞机主体侧面上的蒙皮面板以表面接合的方式接合,并且与从飞机机翼向上延伸的立柱面板以表面接合的方式接合。多个紧固件延伸穿过接头面板和立柱面板,并延伸穿过接头面板和蒙皮面板。该多个紧固件将接头面板附接到蒙皮面板,并将接头面板附接到立柱面板,从而将蒙皮面板附接到立柱面板。在穿过接头面板和立柱面板钻出紧固件孔以将接头面板附接到立柱面板后,可以从立柱面板上去除接头面板。这样便于进入穿过立柱面板钻出的紧固件孔,以去除紧固件孔的毛刺。
JOINT JOINING AN AIRCRAFT WING TO AN AIRCRAFT BODY
将飞机机翼连接到飞机主体的接头
2021-06-22
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |