Abstract: 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.

Abstract: The invention relates to a device for spatially aligning at least two large-format subassembly components, in particular at least one side shell 7, 8, at least one upper shell 12, at least one lower shell 11 and/or at least one floor structure, relative to each other for integrating a component, in particular a fuselage section of an aircraft, comprising: a) at least two positioning devices for taking up in each case a subassembly component, in particular at least two side shell positioners 2, 3, at least one upper shell positioner 5 and/or at least one lower shell positioner 4, b) at least one measuring device for acquiring a multitude of measured data, in particular of positioning data relating to the subassembly components and/or to the positioning devices, c) at least one control and/or regulating device 19, in particular at least one CNC control system, and d) at least one neuronal network 20.