Device for spatially orienting at least two subgroup components and method
First Claim
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1. A device for spatially aligning at least two 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 positioning device a large-format 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 data including positioning data relating to the large-format subassembly components and/or to the positioning devices;
c) at least one control and/or regulating device, including at least one CNC (Computer Numerical Control) control system for controlling a simultaneous linear traverse movement of the positioning devices of the large-format subassembly components until a desired position has been reached, wherein the desired position is a position for tacking and/or joining the at least two large-format subassembly components; and
d) at least one neuronal network for controlling a simultaneous movement of the positioning devices of the large-format subassembly components to assume a desired geometric shape which is predefined in a CAD (Computer Aided Design) component data.
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Abstract
A device for spatially aligning at least two large-format subassembly components, particularly at least one side shell, at least one upper shell, at least one lower shell and/or at least one floor structure, relative to each other for integrating a component, particularly a fuselage section of an aircraft, is provided which includes:
- at least two positioning devices for taking up in each case a subassembly component, particularly at least two side shell positioners, at least one upper shell positioner and/or at least one lower shell positioner,
- at least one measuring device for acquiring a multitude of measured data, particularly of positioning data relating to the subassembly components and/or to the positioning devices,
- at least one control and/or regulating device, particularly at least one CNC control system, and
- at least one neuronal network.
Moreover, a method for aligning the subassembly components is also provided.
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Citations
14 Claims
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1. A device for spatially aligning at least two 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 positioning device a large-format 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 data including positioning data relating to the large-format subassembly components and/or to the positioning devices; c) at least one control and/or regulating device, including at least one CNC (Computer Numerical Control) control system for controlling a simultaneous linear traverse movement of the positioning devices of the large-format subassembly components until a desired position has been reached, wherein the desired position is a position for tacking and/or joining the at least two large-format subassembly components; and d) at least one neuronal network for controlling a simultaneous movement of the positioning devices of the large-format subassembly components to assume a desired geometric shape which is predefined in a CAD (Computer Aided Design) component data. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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12. A method for spatially aligning at least two large-format subassembly components relative to each other for integrating a fuselage section of an aircraft with at least two positioning devices, comprising the following steps:
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a) inserting a large format subassembly component in each one of at least two positioning devices, 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) simultaneously moving the positioning devices under control of at least one neuronal network and of at least one measuring device until a predetermined desired geometric shape which is predefined in a CAD (Computer Aided Design) component data has been reached; c) acquiring positioning data of at least two large-format subassembly components and/or of the positioning devices by means of a measuring device to determine an actual position; and d) aligning the at least two large-format subassembly components in a controlled manner by at least one control and/or regulating device including at least one CNC (Computer Numerical Control) control system by simultaneously moving the positioning devices through a linear traverse movement based on an actual position of each of the at least two large-format subassembly components acquired by the measuring device and/or by the measuring sensors until a desired position has been reached, wherein the desired position is a position for tacking and/or joining the at least two large format subassembly components. - View Dependent Claims (13, 14)
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Specification