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A method of CNC milling without allowance for aircraft skin

A technology for aircraft skin and CNC milling, applied in milling machine equipment, milling machine equipment details, metal processing equipment, etc., can solve the problems of overall skin deviation, inability to be widely used, large gap between suction cups, etc., and achieve the effect of reducing positioning accuracy requirements.

Active Publication Date: 2017-07-14
SHENYANG AIRCRAFT CORP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] According to the above process, there are the following disadvantages in the skin milling without margin: the development cost of the flexible tooling based on this process is high, and the positioning accuracy of the suction cup of the existing flexible tooling is synthesized by the positioning accuracy of the X-axis, Y-axis, and Z-axis of the support rod
The flexible tooling assembly hole locator relies on workers to manually complete the positioning and locking of the x-axis, y-axis, z-axis, A angle, and C angle. The positioning accuracy of each axis is relatively large, resulting in the relative position of the actual clamped skin and the origin of the tool It is inconsistent with the relative position in the assembly digital model, and the NC machining program is compiled based on the three-dimensional assembly digital model, which will cause the overall deviation of the processed skin compared with the digital model
2) The shape and surface of the skin in the actual clamping and assembly of the digital model are inconsistent. On the one hand, due to the large distance between the suction cups, the surface fitted with the suction cup clamping points as discrete points is difficult to be consistent with the theoretical shape and surface, and the edge difference is even greater ; On the other hand, the suction cup of the flexible tooling can swing with the movement, and the clamping (adsorption) of the suction cup is elastic, which will cause the actual suction cup clamping point to be inconsistent with the discrete points of the shape and surface, and the shape and surface after adsorption are inconsistent with the theoretical inconsistent shape
Based on the above-mentioned deficiencies in many aspects, the existing CNC milling process based on suction cup-type flexible tooling without margin can not be widely used in actual production

Method used

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  • A method of CNC milling without allowance for aircraft skin
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  • A method of CNC milling without allowance for aircraft skin

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Embodiment 1

[0068] Embodiment A suction cup type flexible tooling

[0069] Such as Figure 7-22 Shown is a suction cup-type flexible tooling based on the above method, such as Figure 8 The shown flexible tooling includes a tooling frame, several double-bar support units 10, several four-bar support units 11 and several reference support units 12 arranged on the tooling frame; Figure 8-10 The tooling frame shown has a base 4, on which a connecting bracket 5 is provided, and on the connecting bracket 5, several assembling-type supporting plates 8 are provided, and the following supporting plates 8 and the connecting bracket 5 pass through the fastening assembly 6 and the positioning pin 7 are fastened on the base 4; each conformal support plate 8 is provided with several mounting holes, and the mounting holes are equipped with tensioning sleeves 9, and the connecting rods 2 are sequentially penetrated into the coaxial joints on the conformal support plate 8. In the installation hole, th...

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Abstract

The invention discloses a method for CNC milling and cutting of aircraft skin without allowance. The actual pose and shape point cloud of the skin obtained by three-dimensional scanning of the clamped skin is added to a flexible tooling with a machine-added origin adapter and an assembly hole adapter. In order to obtain the point cloud data of the additional machine-added origin adapter and the assembly hole adapter; use the point cloud fitting technology to fit the assembly hole pose and the tooling origin coordinate system; use the finite element technology to map the theoretical digital-analog milling boundary to the skin point The cloud-shaped surface is used as the milling boundary; the machining origin coordinate system is used as the machining origin, and the milling boundary is used as the processing path to write the NC machining program. The actual processing origin is established by using the CNC machine tool with the machine-added origin adapter as a reference, and the processing is carried out. The process method does not have high requirements on the positioning accuracy of each clamping point, and can greatly simplify the production cost of the flexible tooling.

Description

technical field [0001] The invention relates to the technical field of aircraft skin milling without margin, in particular to a method for CNC milling without margin of aircraft skin. Background technique [0002] The traditional aircraft skin margin removal method is to fix the skin blank on a special trimming die, and the workers manually operate the cutting equipment to trim the edge according to the model, which requires a large amount of labor and low trimming accuracy. Therefore, the milling and cutting of skin blanks by adopting the skin non-residue CNC milling process based on suction cup-type flexible tooling (flexible tooling) can significantly improve the quality and efficiency of milling and reduce the number of tooling, and is the main method to achieve no-residue milling of skin . [0003] However, the main process of the existing sucker-type flexible tooling for skin without margin CNC milling process is as follows: 1. Digital-analog virtual assembly: accordi...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23C3/00B23C3/08
Inventor 白新宇迟彩楼白继鹏
Owner SHENYANG AIRCRAFT CORP
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