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Device and method for spatially orienting at least two subassembly parts

A technology of sub-assembly and positioning device, which is applied in the field of component device and base plate frame structure, which can solve the problems of long assembly time and so on.

Inactive Publication Date: 2015-08-26
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The above-mentioned deficiencies in the practice used hitherto in the assembly process of fuselage sections or in the devices used for this purpose lead to long assembly times

Method used

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  • Device and method for spatially orienting at least two subassembly parts
  • Device and method for spatially orienting at least two subassembly parts

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Experimental program
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Embodiment Construction

[0063] figure 1 A schematic diagram of a device according to the invention is shown.

[0064] The device 1 comprises in particular two side housing positioners 2 , 3 , a lower housing positioner 4 and an upper housing positioner 5 . In addition, at least one additional positioning means can be designed, for example, to enable at least one floor structure ( figure 1 not shown) aligned display frame. Furthermore, two working platforms or boom lifts (not shown for clarity) arranged on both sides of the upper housing positioner 5 are provided, so that manual intervention by an operator is possible. Coordinate system 6 means figure 1 Spatial location of all components shown. Due to the size of the subassembly parts picked up by the positioners 2-5, in a preferred embodiment variant of the device 1, each positioner is followed by at least one other positioner, so that in the direction of the x-axis offset.

[0065] On the two side housing positioners 2, 3, the side housings 7,...

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PUM

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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.

Description

technical field [0001] The invention relates to a method for spatially aligning at least two large-scale subassembly parts, in particular at least one side housing, at least one upper housing, at least one lower housing and / or at least one floor frame structure, relative to each other A device for integrating components, in particular of aircraft fuselage sections. [0002] In addition, the invention relates to a method of spatially aligning at least two subassembly parts. Background technique [0003] In modern aircraft construction, fuselage units are usually manufactured using the so-called partial assembly process. In this process, subassembly parts such as side shells, upper and lower shells and the floor structure as well as applicable other system components such as technical equipment systems are integrated together to form fuselage sections. A complete fuselage unit of the aircraft is then formed by a plurality of fuselage sections arranged one behind the other. ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23P19/00B64F5/00
CPCB23P19/10B64F5/0009B23P2700/01B64F5/10
Inventor U.施塔克J.施里克尔W.布兰特
Owner AIRBUS OPERATIONS GMBH