作者: Wolfgang Brandt , Jörg Schrickel , Ulrich Stark
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摘要: The invention relates to a device for spatially orienting at least two large-size subgroup components, in particular one side shell (7,8), upper (12), lower (11), and/or floor framework, relation each other integrate component, fuselage section of an aircraft, comprising: a) positioning apparatuses accommodating component each, positioners (2,3), positioner (5), (4), b) measuring apparatus detecting plurality measurement data, position data the components apparatuses, c) control regulating (19), CNC controller, and d) neural network (20). (20) integrated according into allows be brought specified target geometry by means simultaneous movement shortest amount time with high accuracy. (19) is used preferably subsequently orient simultaneously executed linear movements positioners. further method components.