Processing system for aircraft structural components
AssigneeBroetje-Automation GmbH
InventorsNils Varrelmann, Volker Neemann
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AssigneeBroetje-Automation GmbH
InventorsNils Varrelmann, Volker Neemann
Estimating the term…
A processing installation for aircraft structural components having a processing station comprising a clamping frame, wherein the clamping frame extends along a station longitudinal axis which extends in a longitudinal direction, and a processing unit which has an upper tool unit having an upper tool which is orientated along a first tool axis and a lower tool unit having a lower tool which is orientated along a second tool axis, wherein the first tool axis and the second tool axis can be orientated parallel with a vertical direction which is angular, in particular orthogonal, relative to the longitudinal direction, wherein in at least one processing position of the upper tool and in at least one processing position of the lower tool the first tool axis and the second tool axis are orientated coaxially relative to each other, and wherein the lower tool is supported on a lower tool carrier.
A processing installation for aircraft structural components comprising a processing station comprising a clamping frame for receiving an aircraft structural component which is intended to be processed, wherein the clamping frame extends along a station longitudinal axis which extends in a longitudinal direction, and a processing unit for processing the aircraft structural component which has an upper tool unit having an upper tool which is orientated along a first tool axis and a lower tool unit having a lower tool which is orientated along a second tool axis, wherein the first tool axis and the second tool axis are or can be orientated parallel with a vertical direction which is angular relative to the longitudinal direction, wherein in at least one processing position of the upper tool and in at least one processing position of the lower tool the first tool axis and the second tool axis are orientated coaxially relative to each other, and wherein the lower tool is supported on a lower tool carrier,
A processing installation for aircraft structural components comprising a processing station comprising a clamping frame for receiving an aircraft structural component which is intended to be processed, wherein the clamping frame extends along a station longitudinal axis which extends in a longitudinal direction, and a processing unit for processing the aircraft structural component which has an upper tool unit having an upper tool which is orientated along a first tool axis and a lower tool unit having a lower tool which is orientated along a second tool axis, wherein the first tool axis and the second tool axis are or can be orientated parallel with a vertical direction which is angular relative to the longitudinal direction, wherein in at least one processing position of the upper tool and in at least one processing position of the lower tool the first tool axis and the second tool axis are orientated coaxially relative to each other, and wherein the lower tool is supported on a lower tool carrier,
Dependencies are inferred from the claim text.