Bolted joint of the cover of an access opening in an aircraft lifting surface
    1.
    发明申请
    Bolted joint of the cover of an access opening in an aircraft lifting surface 审中-公开
    在飞机提升表面上的进入开口的盖的螺栓接头

    公开(公告)号:US20130280008A1

    公开(公告)日:2013-10-24

    申请号:US13845272

    申请日:2013-03-18

    CPC classification number: B64C3/26 B64C1/1446 B64C3/34 F16B5/025

    Abstract: A bolted joint for connecting a cover of an opening in a primary structure of a lifting surface of an aircraft to the primary structure. The bolted joint includes two first bolted joints on either side of a symmetry axis of the cover arranged without any lateral clearance, two second bolted joints on either side of the symmetry axis on the side of the cover opposite to that of the two first bolted joints, arranged without any lateral clearance in the holes of the primary structure and with a linear lateral clearance in the holes of the cover; a plurality of third bolted joints along the border of the cover arranged without any lateral clearance in the holes of the primary structure and with a radial clearance in the holes of the cover.

    Abstract translation: 用于将飞行器的提升表面的主结构中的开口的盖连接到主结构的螺栓接头。 螺栓接头包括两个第一螺栓接头,其位于盖的对称轴线的任一侧,其布置为没有任何侧向间隙,两个第二螺栓连接在对称轴线的两侧上,与盖子的两个第一螺栓接头 在第一结构的孔中没有任何侧向间隙并且在盖的孔中具有线性侧向间隙; 沿着盖的边界的多个第三螺栓接头,其布置成在主结构的孔中没有任何侧向间隙,并且在盖的孔中具有径向间隙。

Patent Agency Ranking