The invention relates to a processing installation for aircraft structural components (2) having at least one processing station (3, 4), wherein the processing station (3, 4) has a clamping frame (7, 8) which extends along a longitudinal station axis (5, 6) for receiving the aircraft structural component (2) which is intended to be processed in each case and a processing unit (9, 10), preferably a riveting unit, for processing the aircraft structural component (2) and wherein the clamping frame (7, 8) is articulated so as to be adjustable in terms of height and pivotable to two positioning towers (11, 12) which are arranged in a vertical tower plane (13). It is proposed that there be provided transversely relative to the tower plane (13) a transverse offset of the clamping frame (7, 8) which enables an aircraft structural component (2) to be loaded onto and/or unloaded from the clamping frame (7, 8) along the tower plane (13) and at least one positioning tower (11, 12) to be passed laterally.
PROCESSING SYSTEM FOR AIRCRAFT STRUCTURAL COMPONENTS
2017-11-23
Patent
Elektronische Ressource
Englisch