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Reverse identification method of residual stress distribution of titanium alloy thin-walled parts based on deformation test

A residual stress and deformation testing technology, applied in the direction of improvement of process efficiency, special data processing applications, instruments, etc., can solve problems such as practical application difficulties, achieve good application prospects, less characterization coefficients, and fast prediction speed

Active Publication Date: 2022-05-31
NORTHWESTERN POLYTECHNICAL UNIV
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  • Application Information

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Problems solved by technology

[0004] The purpose of the present invention is to provide a reverse identification method of residual stress distribution of titanium alloy thin-walled parts based on deformation test, so as to solve the problem that the existing polynomial representation model of residual stress is difficult in practical application

Method used

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  • Reverse identification method of residual stress distribution of titanium alloy thin-walled parts based on deformation test
  • Reverse identification method of residual stress distribution of titanium alloy thin-walled parts based on deformation test
  • Reverse identification method of residual stress distribution of titanium alloy thin-walled parts based on deformation test

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Embodiment

[0098] 1. Design a single-factor titanium alloy end milling test plan. The test piece is a rectangular thin plate of titanium alloy, L=160mm, E=114GPa, I=20×2 3 / 12=13.3mm 4 , see workpiece and dimensions Figure 6. The upper and lower surfaces of the test piece are processed by wire cutting. The tool used is a K44φ10mm uncoated end mill with a helix angle of 40°. The front and rear angles of the bottom edge and side edge are the same. R=0.2mm; the milling method is down milling, dry cutting without lubrication.

[0099] Table 4.1.1 shows the specific milling experimental parameters, and the specific scheme design and test results are shown in Table 4.1.2.

[0100] Table 4.1.1 Milling experimental parameters

[0101]

[0102] Table 4.1.2 Residual stress on TC4 end milling surface

[0103]

[0104]

[0105] A hyperbolic tangent function model of the end milling residual stress is established; the end milling parameters are corresponding to the hyperbolic tangent f...

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Abstract

The invention discloses a method for reverse identification of residual stress distribution of titanium alloy thin-walled parts based on deformation test: step 1, establishing an end milling residual stress hyperbolic tangent function model; corresponding end milling parameters to the end milling residual stress hyperbolic In the tangent function model, the mapping relationship between the two is established; step 2, according to the hyperbolic tangent function model of the end milling residual stress in step 1, the induced bending moment model of the end milling residual stress of thin-walled parts is established, thereby deriving the end milling Theoretical deformation deflection of residual stress, establish the corresponding relationship between the end milling residual stress hyperbolic tangent function model and the theoretical deformation deflection; The mapping relationship obtained in step 1 and the corresponding relationship obtained in step 2 establish a reverse identification algorithm for milling residual stress. It solves the problem that the existing residual stress polynomial characterization model is difficult in practical application.

Description

technical field [0001] The invention belongs to the field of residual stress deformation control of titanium alloy cutting, and in particular relates to a reverse identification method of residual stress distribution of titanium alloy thin-walled parts based on deformation test. Background technique [0002] Due to the advantages of good comprehensive mechanical properties and process properties, titanium alloys are mainly used to make special load-bearing parts with large loads and high temperatures in aircraft structures, such as engine load-bearing frames, pylons, and landing gear compartment frames. Under the joint action of various factors, residual stress will inevitably be generated when titanium alloy is processed and applied. The formation of processing residual stress is the plastic deformation of the internal part of the material under the joint action of mechanical force and thermal effect. Due to the uncoordinated change in the volume of the metallographic struc...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/20G06F30/18G06F119/14G06F111/08
CPCG06F30/20G06F30/18G06F2119/14G06F2111/08Y02P10/20
Inventor 任军学刘强强周金华王宗园
Owner NORTHWESTERN POLYTECHNICAL UNIV
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