| 摘要 |
A device for spatially aligning at least two large-format subassembly components, particularly at least one side shell, at least one upper shell, at least one lower shell and/or at least one floor structure, relative to each other for integrating a component, particularly a fuselage section of an aircraft, is provided which includes: at least two positioning devices for taking up in each case a subassembly component, particularly at least two side shell positioners, at least one upper shell positioner and/or at least one lower shell positioner, at least one measuring device for acquiring a multitude of measured data, particularly of positioning data relating to the subassembly components and/or to the positioning devices, at least one control and/or regulating device, particularly at least one CNC control system, and at least one neuronal network. Moreover, a method for aligning the subassembly components is also provided. |
