Mobile positioning device for rear parts of aircraft products

Abstract

The invention relates to a movable positioning device for a rear section part of an aircraft product. The movable positioning device comprises a first movable positioning device, a second movable positioning device, a third movable positioning device and a fourth movable positioning device, wherein the first movable positioning device comprises a first guide rail and a first movable positioning unit; the second movable positioning device comprises a second guide rail and a second movable positioning unit; the third movable positioning device comprises a third guide rail and a third movable positioning unit; the fourth movable positioning device comprises a fourth guide rail and a fourth movable positioning unit; the first movable positioning device and the second movable positioning device are arranged oppositely in a first direction; the third movable positioning device and the fourth movable positioning device are arranged oppositely in a second direction; the first direction is perpendicular to the second direction; the first movable positioning device, the second movable positioning device, the third movable positioning device and the fourth movable positioning device can move along the corresponding guide rails in the second direction respectively.

Description

technical field [0001] The invention relates to an automatic manufacturing equipment, in particular to a mobile positioning device for the rear part of an aircraft product. Background technique [0002] At present, the assembly of aircraft mainly relies on traditional manual assembly methods, combined with some targeted control measures, which can improve the quality of aircraft assembly to a certain extent, but there is still a considerable gap from the demanding assembly quality technical indicators of advanced aircraft, mainly reflected in: large size The assembly accuracy of the frame-beam frame is not easy to guarantee. Since the maximum size of the frame parts is more than 4 meters, the deformation of the parts during the manufacturing and assembly process is relatively large, and the assembly process lacks effective detection and control measures, which cannot meet the technical requirements of the design; composite material / titanium alloy, composite material / aluminum...

AI Technical Summary

Problems solved by technology

[0002] At present, the assembly of aircraft mainly relies on traditional manual assembly methods, combined with some targeted control measures, which can improve the quality of aircraft assembly to a certain extent, but there is still a considerable gap from the demanding assembly quality technical indicators of advanced aircraft, mainly reflected in: large size It is not easy to guarantee the assembly accuracy of the frame beam frame

Since the maximum size of the frame parts is more than 4 meters, the deformation of the parts during the manufacturing and assembly process is relatively large, and the assembly process lacks effective detection and control measures, which cannot meet the technical requirements of the design; composite material / titanium alloy, composite material / aluminum alloy It is very difficult to make holes in the laminated structure. Manual hole making requires extremely high operating skills of workers, and the hole making efficiency is low. It is prone to layering of composite materials, elliptical diameters, and connector heads caused by inclined hole positions and inaccurate nesting depths. The unevenness of the surface is out of tolerance, seriously affecting the performance of the aircraft

[0003] The current situation of aircraft assembly shows that traditional manual assembly technology can no longer meet the assembly quality requirements of advanced aircraft, and it is necessary to fundamentally change the assembly technology, and digital assembly has become an inevitable choice

The key part of automatic hole-making digital assembly, the assembly of the rear parts of the existing aircraft products adopts closed tooling, but due to the problem of space interference, the automatic hole-making with CNC machine tools cannot be realized. Therefore, the layout of the existing closed tooling must be modified , to meet the operating space required for automatic hole making

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