FIELD: machine building.
SUBSTANCE: invention can be used in processing aircraft structural components (2). Processing station (3) comprises clamping frame (4) and processing module (5). Module (5) has upper tool module (11) with upper tool (13) and lower tool module (14) with lower tool (15). First and second tool axes are oriented parallel to vertical direction (Z) at an angle to longitudinal direction (X). At least in one processing position of upper tool (13) and at least in one processing position of lower tool (15) first and second tool axes are oriented coaxially to each other. Lower tool (15) is installed on the lower tool holder (17). At least in one processing position of upper tool (13) and/or in at least one machining position of lower tool (15), the corresponding tool axis does not pass coaxially to axis (18) of the lower tool holder.
EFFECT: as a result, the installation dimensions are reduced in the vertical direction.
16 cl, 3 dwg
