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Aircraft wall panel digitalization processing and assembling system

An aircraft wall panel and assembly system technology, applied in aircraft assembly, aircraft parts, transportation and packaging, etc., can solve the problems of multiple hoisting, low production efficiency, long procurement cycle, etc., to improve processing efficiency and high functional integration. , The effect of convenient manual operation

Pending Publication Date: 2017-12-22
大连四达高技术发展有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, there is still a blank in the field of automatic hole-making and riveting of large aircraft in China. In the process of hole-making in the skin of large-scale aircraft, domestic manufacturers are limited to small-scale flexible track-type hole-making equipment. Among them, it needs to be hoisted multiple times, there is a problem of repeated positioning, the production efficiency is low, and due to structural reasons, such equipment is often unable to integrate functions such as glue coating, aperture detection, pressure riveting, and tool change at the end, which has certain limitations. It is difficult to greatly improve the efficiency of hole making and riveting
To achieve faster hole-making and riveting efficiency, large-scale aircraft hole-making and riveting equipment is required. At present, most of the large-scale hole-making equipment used by domestic aircraft manufacturers are purchased from abroad, and the cost is relatively high, and the procurement cycle is long. Inconvenient service

Method used

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  • Aircraft wall panel digitalization processing and assembling system
  • Aircraft wall panel digitalization processing and assembling system
  • Aircraft wall panel digitalization processing and assembling system

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Embodiment Construction

[0017] The aircraft panel digital processing assembly system of the present invention, such as figure 1 As shown, the hole-making and riveting system of the lower wall is composed of three parts: the skin side execution system, the stringer side execution system and the positioning tooling.

[0018] The tooling part of the hole making and pressing riveting system of the lower wall plate is as follows: figure 2 As shown, it is mainly composed of a tooling platform 5, a lifting platform 6, a frame positioning component 7, a skin positioning component 8, a multifunctional working ladder 10, and a skin tensioning component 11. The skin positioning tooling 2 includes a tooling platform 5, a lifting platform 6. The frame positioning assembly 7 and the frame 9, the tooling platforms 5 on both sides are installed on the ground 4, the two ends of each frame 9 are installed on the tooling platforms 5 on both sides through the frame positioning assembly 7, the frame 9 is arc-shaped, fro...

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PUM

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Abstract

The invention discloses an aircraft wall panel digitalization processing and assembling system. The system comprises a skin side execution system, a stringer side execution system and a skin locating tool, wherein the skin locating tool comprises a tool platform, a lifting platform, a frame locating component, a skin locating component, a multifunctional working ladder, a skin tension component and a frame; the skin side execution system comprises a tool body, an arc gantry and a skin side tail end executor; the stringer side execution system comprises a base, a stringer side tail end executor, stand pillars, slide bases and slide rails. According to the aircraft wall panel digitalization processing and assembling system, drilling and rivet pressing are integrated, and compared with a D-type gantry, the arc gantry is simpler in algorithm. Regarding the maximal processing range, a 180-degree super wall panel can be processed; the function integration level is high, and the aircraft wall panel digitalization processing and assembling system integrates the functions of drilling, dimpling, bore diameter detection, gumming, pegging, rivet pressing, normal searching, cutter changing, off-line programming, simulation and the like. An automatic locating tool is assembled, the liftable platform is assembled at the bottom of the tool, manual operation is facilitated, that the equipment and the like pass through the bottom of the tool is not influenced either, and the processing efficiency is greatly improved.

Description

technical field [0001] The invention relates to the field of automatic hole-making and riveting equipment for aircraft, in particular to the hole-making and riveting technology for large aircraft wall panels. Background technique [0002] At present, there is still a blank in the field of automatic hole-making and riveting of large aircraft in China. In the process of hole-making in the skin of large-scale aircraft, domestic manufacturers are limited to small-scale flexible track-type hole-making equipment. Among them, it needs to be hoisted multiple times, there is a problem of repeated positioning, the production efficiency is low, and due to structural reasons, such equipment is often unable to integrate functions such as glue coating, aperture detection, pressure riveting, and tool change at the end, which has certain limitations. It is difficult to greatly improve the efficiency of hole making and riveting. To achieve faster hole-making and riveting efficiency, large-s...

Claims

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Application Information

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IPC IPC(8): B64F5/10B23P15/00
CPCB64F5/10B23P15/00B23P2700/01Y02T50/40
Inventor 李东栓
Owner 大连四达高技术发展有限公司
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