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Method for predicting milling residual stress field of titanium alloy

A residual stress and prediction method technology, applied in special data processing applications, instruments, electrical digital data processing, etc., can solve problems such as poor prediction accuracy, heavy testing workload, and difficult control of residual stress field, achieving high accuracy, Effects of rapid prediction and robust design and analysis methods

Active Publication Date: 2017-03-22
NORTHWESTERN POLYTECHNICAL UNIV
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Problems solved by technology

[0007] The present invention aims at the problems of difficulty in controlling the residual stress field, heavy testing workload, and poor prediction accuracy in the above-mentioned existing milling process, and proposes a method for predicting the residual stress field of titanium alloy milling based on an exponential decay function, and realizes the prediction of the titanium alloy milling residual stress field. Prediction of residual stress field in alloy milling, and then guide the selection of titanium alloy milling process parameters

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  • Method for predicting milling residual stress field of titanium alloy
  • Method for predicting milling residual stress field of titanium alloy
  • Method for predicting milling residual stress field of titanium alloy

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Embodiment 1

[0055] Embodiment 1, a kind of titanium alloy milling residual stress field prediction method based on exponential decay function

[0056] The prediction method of this embodiment is carried out according to the following steps:

[0057] Step 1: Determine the exponential decay function model of the milling residual stress field

[0058] After milling, the surface layer of titanium alloy is in the state of residual compressive stress, and the residual compressive stress gradually decreases with the increase of the depth below the surface, and reaches the state of residual stress in the matrix. Therefore, an exponential decay function is proposed to describe the milling residual compressive stress curve.

[0059] σ(h)=Ae -λh

[0060] where σ is the residual stress; h is the subsurface depth; A is the initial value of the residual stress; λ is the exponential decay coefficient, which determines how fast the residual compressive stress field decays to a stable value.

[0061] ...

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Abstract

The invention relates to a method for predicting a milling residual stress field of titanium alloy. The method can predict the milling residual stress field of the titanium alloy based on exponential decay functions and includes the main steps: 1, determining an exponential decay function model of a milling residual stress field; 2, determining a relation model between a residual stress field control factor and a milling process parameter; 3 selecting the milling process parameter and performing encoding; 4, designing a test scheme, and performing a milling test; 5, testing the residue stress field; 6 solving the residual stress field control factor. The method uses the milling process parameter as an input condition, and can acquire distribution of the residue stress along a surface in the milling process parameter by solving a model coefficient, is simple and reliable, is fast in prediction speed, is high in accuracy, can avoid lots of complex tests, can avoid difficulties of the finite element method and the physical analytical method, and can be used by mass engineering and technical staff.

Description

technical field [0001] The invention belongs to the technical field of metal material machining, and in particular relates to a method for predicting the residual stress field of TC17 titanium alloy milling based on an exponential decay function. Background technique [0002] Titanium alloy material has excellent properties such as light weight, high strength, high temperature resistance and fatigue resistance. It is an important metal material for manufacturing major equipment in aerospace, national defense and other fields and key parts in new strategic weapons. In the structural design of new aero-engines, complex thin-walled components are widely used in order to achieve the purpose of reducing weight and increasing efficiency. With the continuous improvement of aero-engine bypass ratio, thrust-to-weight ratio and service life, the structure of thin-walled components becomes more complex, the material is more difficult to process, and the requirements for shape accuracy ...

Claims

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Application Information

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IPC IPC(8): G06F17/50
CPCG06F30/20
Inventor 姚倡锋谭靓张定华任军学田荣鑫周征张吉银傅新强周菲
Owner NORTHWESTERN POLYTECHNICAL UNIV
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