Titanium alloy skin laser cutting method based on flexible supporting device

A flexible support and laser cutting technology, which is applied in laser welding equipment, metal processing equipment, manufacturing tools, etc., can solve the problems that affect the cutting accuracy of parts, the parts and fixtures cannot be tightly fitted, and occupy a large inventory area, so as to reduce scrap rate and repair rate, reduce the labor intensity of workers, and reduce the effect of production costs

Inactive Publication Date: 2014-09-03
SHENYANG AIRCRAFT CORP
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AI Technical Summary

Problems solved by technology

[0003] In order to solve the problems and deficiencies in the prior art, the present invention provides a titanium alloy skin laser cutting method based on a flexible support device, which uses the cooperation of a flexible support device and a five-coordinate laser cutting machine to cut titanium alloy parts, It not only solves the problem that the titanium alloy skin part and the fixture cannot be tightly fitted, which affects the cutting accuracy of the part, but also solves the problem that the remaining part of the titanium alloy skin part is unsupported, and it is easy to cause the part to vibrate during the falling process, resulting in the edge of the part The problem of poor cutting quality. At the same time, the flexible support device has versatility, which avoids the defects of the existing special tooling such as a large number of types, large volume, large inventory area, and high cost.

Method used

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  • Titanium alloy skin laser cutting method based on flexible supporting device

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Embodiment Construction

[0019] Such as figure 1 Shown is a schematic diagram of the flexible supporting device and the laser cutting of the titanium alloy skin. The flexible supporting device includes a platform 1 , holes 5 evenly distributed on the platform 1 , positioning rods 4 and supporting rods 6 placed in the holes 5 .

[0020] A kind of laser cutting method of titanium alloy skin based on flexible supporting device, comprises the steps:

[0021] 1) Design the digital model of the titanium alloy skin 3 according to the drawing requirements of the titanium alloy skin 3, design three lugs on the digital model of the titanium alloy skin 3, the three lugs respectively have a positioning hole, and three positioning holes The projection of the hole center on the XY plane is an integer multiple of 100mm in the X and Y directions, and the process digital model of the titanium alloy skin 3 is generated;

[0022] 2) Based on the process digital model, manufacture a titanium alloy skin 3 with three lugs...

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Abstract

The invention provides a titanium alloy skin laser cutting method based on a flexible supporting device. According to the method, the flexible supporting device and a five-coordinate laser cutting machine are used in cooperation for cutting titanium alloy parts, not only is the problem that because the titanium alloy skin parts can not be tightly attached to a clamp, the part cutting precision is influenced solved, but also the problems that because the allowance portions of the titanium alloy skin parts can not be supported, the parts are prone to vibrating in the part falling process, and the cutting quality of the edges of the parts is poor are solved. Meanwhile, the flexible supporting device is universal, and the defects that existing special tools are various in variety and number, large in size and occupied inventory area and high in cost are overcome.

Description

technical field [0001] The invention relates to the field of processing aircraft titanium alloy skin parts, in particular to a laser cutting method for titanium alloy skin parts based on a flexible support device. Background technique [0002] The design of aircraft zigzag titanium alloy skin puts forward higher requirements for the edge quality and precision of parts. Traditionally, laser cutting fixtures are used for laser cutting of parts. However, in actual production, due to factors such as high rigidity of titanium alloy parts and tooling manufacturing errors, etc. , the part and the fixture cannot be tightly fitted, which affects the cutting accuracy of the part; at the same time, there is no support for the spare part of the part, which may easily cause the part to vibrate during the falling process, resulting in poor cutting quality of the edge of the part, which cannot meet the inspection requirements, and a large number of subsequent manual trimming The work great...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23K26/38B23K26/40B23K26/70
CPCB23K26/38B23K26/40B23K26/702B23K2103/08B23K2103/14
Inventor 李丁翟南李铭张一丁
Owner SHENYANG AIRCRAFT CORP
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