发明名称 Determinant wing assembly
摘要 A method and apparatus for manufacturing wings includes a fixture that holds wing panels for drilling and edge trimming by accurate numerically controlled machine tools using original numerical part definition records, utilizing spatial relationships between key features of detail parts or subassemblies as represented by coordination features machined into the parts and subassemblies, thereby making the parts and subassemblies intrinsically determinant of the dimensions and contour of the wing. Spars are attached to the wing panel using the coordination holes to locate the spars accurately on the panel in accordance with the original engineering design, and in-spar ribs are attached to rib posts on the spar using accurately drilled coordination holes in the ends of the rib and in the rib post. The wing contour is determined by the configuration of the spars and ribs rather than by any conventional hard tooling which determines the wing contour in conventional processes.
申请公布号 US6314630(B1) 申请公布日期 2001.11.13
申请号 US19980155251 申请日期 1998.09.21
申请人 THE BOEING COMPANY 发明人 MUNK CLAYTON L.;NELSON PAUL E.;STRAND DAVID E.
分类号 B23Q3/06;B23P21/00;B23Q17/00;B25B5/12;B25B5/16;B25B11/00;B64C3/18;B64C3/26;B64F5/00;G05B19/401;G05B19/408;G05B19/44;(IPC1-7):B23Q17/00;G01M19/00 主分类号 B23Q3/06
代理机构 代理人
主权项
地址