| 摘要 |
The invention relates to a device for spatially orienting at least two large-size subgroup 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 framework, in relation to each other to integrate a component, in particular a fuselage section of an aircraft, comprising: a) at least two positioning apparatuses for accommodating one subgroup component each, 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 apparatus for detecting a plurality of measurement data, in particular position data of the subgroup components and/or of the positioning apparatuses, c) at least one control and/or regulating apparatus (19), in particular at least one CNC controller, and d) at least one neural network (20). The neural network (20) integrated according to the invention into the device allows the subgroup components to be brought into a specified target geometry by means of simultaneous movement of the positioning apparatuses in the shortest amount of time and with high accuracy. The control and/or regulating apparatus (19) is used preferably to subsequently orient the subgroup components in relation to each other by means of simultaneously executed linear movements of the positioners. The invention further relates to a method for orienting subgroup components. |
