FIELD: instrumentation.
SUBSTANCE: invention relates to device (1) for spatial orientation of two large-sized components of fuselage sections. Particularly, it covers the orientation of at least one side shell (7, 8), at least one top shell (12), at least one bottom shell (11) and/or at least on floor carcass relative to each other for assembly of aircraft fuselage. This device comprises a) at least two side shell positioning devices (2, 3), at least one top shell positioning device (5) and/or at least one bottom shell positioning device (4). b) At least one measuring device is used to define the multiple data of measurements, particularly, about the position of section components and/or positioning devices. c) At least one control device (19) is used for, particularly, CNC control as well as d) at least one neuronal circuit (20). Said control device (19) is designed, preferably, for final orientation of section components relative to each other along with linear displacement of positioning devices.
EFFECT: application of neuronal circuit (20) allows simultaneous transfer of positioning devices and their precise location to preset design configuration.
15 cl, 2 dwg
