Method for predicting low-cycle fatigue life of titanium alloy material based on surface integrity

A technology of surface integrity and low cycle fatigue, applied in the direction of applying stable tension/pressure to test the strength of materials, it can solve the problems of high performance parameters and inability to meet the needs of engineering development, and achieve simplified prediction models and rapid low cycle fatigue. Effects of life prediction, improved stability and accuracy

Active Publication Date: 2015-12-30
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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Problems solved by technology

[0004] With the development of modern science and technology, the structure of titanium alloy mechanical products is becoming more and more complex, the performance parameters are getting higher and higher, and the working environment conditions are more severe. The contradiction between the traditional fatigue life prediction method of titanium alloy and engineering practice is gradually emerging. The reason is that The traditional deterministic methods cannot describe the objectively existing uncertain phenomena in engineering well.
Under actual service conditions, the workpiece is often subjected to uncertain loading conditions, therefore, the traditional fatigue life prediction method based on loading conditions will not be able to meet the needs of engineering development

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  • Method for predicting low-cycle fatigue life of titanium alloy material based on surface integrity
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  • Method for predicting low-cycle fatigue life of titanium alloy material based on surface integrity

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Embodiment Construction

[0025] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0026] The invention is a method for predicting the low cycle fatigue life of titanium alloy materials based on surface integrity, the process of which is as follows: figure 1 As shown, the implementation steps of the present invention are described in detail below with the TC4-DT titanium alloy material as an example:

[0027] Step 1: It is judged that TC4-DT is a new type of titanium alloy material, so you can go to step 2;

[0028] Step 2: Perform finite element analysis on the structure of TC4-DT workpiece to obtain its stress distribution and judge whether it is low cycle fatigue;

[0029] Step 3: It is found that the TC4-DT workpiece structure produces plastic strain at the dangerous point, so it can be judged that it is low cycle fatigue, and enter step 4;

[0030] Step 4: Set different cutting parameters, including cutting speed, fe...

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Abstract

The invention discloses a method for predicting the low-cycle fatigue life of a titanium alloy material based on the surface integrity. The low-cycle fatigue failure mode of the titanium alloy material under the pulling-pressing loading condition is considered, index parameters of the surface integrity serve as bases, a polynomial regression model is combined with a sine and cosine regression model, a predicting model for evaluating the low-cycle fatigue life of the titanium alloy material by adopting a combination of the surface roughness Ra and the maximum surface residual main stress sigmar is built, and finally a method for predicting the low-cycle fatigue life of the titanium alloy material based on the surface integrity is provided. By means of the method, the low-cycle fatigue life of the titanium alloy material can be easily, rapidly and accurately predicted, theoretical bases can be provided for reliable design of parts, practical production can be guided, and the certain engineering application value can be achieved.

Description

technical field [0001] The present invention relates to the prediction of the fatigue life of titanium alloy materials under tensile and compressive loads, in particular to a low-cycle fatigue aging method for titanium alloy materials based on surface integrity, which is suitable for widely used in automobiles, aerospace, ships and medical treatment Various titanium alloy materials. Background technique [0002] With the wide application of titanium alloys in the aviation industry, automobile industry, shipbuilding industry and medical fields, the problem of low-cycle fatigue damage of titanium alloys has become increasingly prominent, which seriously threatens the safety and reliability of titanium alloy structural parts. The complexity of the service environment and the variability of the load history of large mechanical structures such as aerospace equipment, ships, and rail vehicles may lead to sudden failure of the structure and sudden accidents. The safety of large-sc...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N3/08
Inventor 陈明和杜舜尧朱知寿王新南
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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