The invention relates to mirror image fabrication and assembly of aircraft wings. Systems and methods are provided for an assembly line (100) for processing a wing panel (150) of an aircraft. The method includes inputting the wing panels (150) into an assembly line (100) having a plurality of stations (120), the wing panels (150) being oriented such that leading edges (155) are all on a first side (166) of the stations (120) and trailing edges (157) are all on a second side (165) of the stations (120), and advancing the wing panels (150) in a machining direction (181) through the plurality of stations (120), the plurality of stations (120) being oriented such that the leading edges (155) are all on the first side (166) of the stations (120) and the trailing edges (157) are all on the second side (165) of the stations (120). At least a first portion of the station (120) is dedicated to wing panel leading edge (155) machining and a second portion of the station (120) is dedicated to wing panel trailing edge (157) machining.
本公开涉及飞行器机翼的镜像制作和组装。提供了用于对飞行器的机翼面板(150)进行加工的组装线(100)的系统和方法。该方法包括将机翼面板(150)输入到组装线(100)中,该组装线(100)具有多个工位(120),机翼面板(150)按照使得前缘(155)全部在工位(120)的第一侧(166)上并且后缘(157)全部在工位(120)的第二侧(165)上的方式来定向,并且将机翼面板(150)在加工方向(181)上推进通过多个工位(120),所述工位(120)的至少第一部分专用于机翼面板前缘(155)加工,并且所述工位(120)的第二部分专用于机翼面板后缘(157)加工。
Mirror fabrication and assembly of aircraft wings
飞行器机翼的镜像制作和组装
2022-05-20
Patent
Elektronische Ressource
Chinesisch
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