The invention relates to profile application of a wire assembly gantry. Systems and methods for assembling sections of a fuselage (12) of an aircraft (10) are provided. The method comprises: pulsing a half-barrel section (24) of the fuselage (12) in a machining direction (199) along a track (110); determining a desired profile (361) of a portion of the half-barrel section (24) using an indexing feature (124) associated with the half-barrel section (24); and applying the desired profile (361) to the half-barrel section (24) using the means for applying the inner mold line (128) and the means for applying the outer mold line (126) when the profile of the half-barrel section (24) differs from the desired profile by outside of a tolerance (361).
本发明涉及线组装机身段的轮廓施加。提供了用于组装飞行器(10)的机身(12)的区段的系统和方法。该方法包括:使所述机身(12)的半机筒区段(24)在加工方向(199)上沿轨道(110)脉动;利用与所述半机筒区段(24)相关联的转位特征(124)来确定所述半机筒区段(24)的一部分的期望轮廓(361);以及当所述半机筒区段(24)的所述轮廓与所述期望轮廓相差处于公差(361)之外时,使用施加内模线(128)的部件和施加外模线(126)的部件将所述期望轮廓(361)施加到所述半机筒区段(24)上。
Profile application of wire assembly gantry
线组装机身段的轮廓施加
2022-05-20
Patent
Electronic Resource
Chinese