发明名称 SYMMETRIC WING RIB WITH CENTER PLANE FASTENED SHEAR TIES
摘要 A symmetrical rib structure and methods are presented. A structural web comprises a web center plane and a plurality of web stiffeners, and is symmetrical about the web center plane. A flange is configured on a periphery of the symmetrical rib structure, and a fastener hole is configured in the flange and comprises a fastener hole centerline aligned with the web center plane. A cutout is configured in the structural web around the fastener hole, and two support columns are coupled to the flange on opposite sides of the cutout.
申请公布号 US2015298790(A1) 申请公布日期 2015.10.22
申请号 US201313923841 申请日期 2013.06.21
申请人 The Boeing Company 发明人 Vanderhoek John David
分类号 B64C3/18;B64F5/00 主分类号 B64C3/18
代理机构 代理人
主权项 1. A symmetrical rib structure comprising: a structural web comprising a plurality of web stiffeners, wherein the structural web and the plurality of web stiffeners are arranged symmetrical about a web center plane such that the symmetrical rib structure has a first side relative to the web center plane and a second side opposite the first side relative to the web center plane; a flange configured on a periphery of the symmetrical rib structure; a fastener hole configured in the flange and comprising a fastener hole centerline aligned with the web center plane; a cutout is configured in the structural web around the fastener hole, wherein the cutout comprises a shear tie cutout and the flange comprises a shear tie foot; and two shear tie support columns are coupled to the flange on opposite sides of the cutout and a structural web chord arranged on an opposite side of the cutout from the flange.
地址 Chicago IL US