DEVICE FOR SPATIALLY ORIENTING AT LEAST TWO SUBGROUP COMPONENTS AND METHOD
First Claim
1. A device for spatially aligning large-format subassembly components, relative to each other for integrating a fuselage section of an aircraft, comprising:
- a) at least two positioning devices for taking up in each case a subassembly component, the at least two positioning devices selected from the group consisting of at least two side shell positioners, at least one upper shell positioner, at least one lower shell positioner, and combinations thereof;
b) at least one measuring device for acquiring a multitude of measured data, the measured date including positioning data relating to the subassembly components and/or to the positioning devices;
c) at least one control and/or regulating device, including at least one CNC control system; and
d) at least one neuronal network.
1 Assignment
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Accused Products
Abstract
The invention relates to a device for spatially aligning at least two large-format subassembly 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 structure, relative to each other for integrating a component, in particular a fuselage section of an aircraft, comprising:
- a) at least two positioning devices for taking up in each case a subassembly component, 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 device for acquiring a multitude of measured data, in particular of positioning data relating to the subassembly components and/or to the positioning devices,
- c) at least one control and/or regulating device 19, in particular at least one CNC control system, and
- d) at least one neuronal network 20.
The neuronal network 20 integrated according to the invention in the device makes it possible by simultaneous moving of the positioning devices to bring the subassembly components in a very short time and with high accuracy to assume a predetermined desired geometric shape. The control and/or regulating device 19 is preferably used for the subsequent alignment of the subassembly components relative to each other by means of simultaneously carried out linear traverse movements of the positioners.
Moreover, the invention relates to a method for aligning subassembly components.
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Citations
14 Claims
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1. A device for spatially aligning large-format subassembly components, relative to each other for integrating a fuselage section of an aircraft, comprising:
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a) at least two positioning devices for taking up in each case a subassembly component, the at least two positioning devices selected from the group consisting of at least two side shell positioners, at least one upper shell positioner, at least one lower shell positioner, and combinations thereof; b) at least one measuring device for acquiring a multitude of measured data, the measured date including positioning data relating to the subassembly components and/or to the positioning devices; c) at least one control and/or regulating device, including at least one CNC control system; and d) at least one neuronal network. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14)
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Specification