Tension torsion steady-state cyclic stress-strain modeling method based on basic mechanics parameters

A technology of cyclic stress and modeling method, which is applied in the direction of testing material strength by applying repetitive force/pulsation force, testing material strength by applying stable tension/compression, and measuring devices, etc., to achieve convenient and fast use, good engineering applicability, Calculate the effect of ease

Active Publication Date: 2020-02-14
XIDIAN UNIV
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Problems solved by technology

[0006] The purpose of the present invention is to address the deficiencies of the above-mentioned prior art, and propose a tensile-torsion steady-state cyclic stress-strain modeling method based on basic mechanical par...

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  • Tension torsion steady-state cyclic stress-strain modeling method based on basic mechanics parameters
  • Tension torsion steady-state cyclic stress-strain modeling method based on basic mechanics parameters
  • Tension torsion steady-state cyclic stress-strain modeling method based on basic mechanics parameters

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Embodiment Construction

[0024] Below in conjunction with accompanying drawing, the present invention will be described in further detail

[0025] Refer to attached figure 1 , to further describe in detail the specific steps of the present invention.

[0026] Step 1. Use the basic mechanical parameters of the material obtained from the static tensile test or query the material manual to determine the model parameters;

[0027] The basic mechanical parameters of the material include tensile strength, yield strength, reduction of area, modulus of elasticity and Poisson's ratio of elasticity. The model parameters include shear modulus of elasticity, cyclic strength coefficient, cyclic strain hardening coefficient and tension-compression fatigue limit.

[0028] The theoretical estimation formula of the shear elastic modulus G is as follows:

[0029]

[0030] In the formula, E is the modulus of elasticity, ν e is the elastic Poisson's ratio.

[0031] The theoretical estimation formula of cycle stre...

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Abstract

The invention provides a tension torsion steady-state cyclic stress-strain modeling method based on basic mechanics parameters. The tension torsion steady-state cyclic stress-strain modeling method based on the basic mechanics parameters comprises the following steps of: step (1). obtaining the basic mechanics parameters of a material; step (2). calculating relevant material parameters by using the basic mechanics parameters; step (3). dispersing load steps, and calculating the stress tensor by using the Hooke's law; step (4). using the yield criterion to judge whether the stress state in step(3) is in the elastic loading stage, if yes, performing the next calculation according to step (6), otherwise, performing the next calculation according to step (5); step (5). calculating an additional strengthening coefficient, a non-proportional band factor, a plastic modulus, plastic strain tensor, bias stress tensor and back stress tensor; and step (6). judging whether the loading is completed, if yes, obtaining the multi-axis steady-state cyclic stress-strain, and otherwise, repeating steps (3) to (6). The tension torsion steady-state cyclic stress-strain modeling method based on the basic mechanics parameters avoids the complicated multi-axial fatigue test, and considers the non-proportional additional strengthening effect of the material, and is convenient for engineering application.

Description

technical field [0001] The invention belongs to the technical field of machinery, and further relates to a modeling method of tension-torsion steady-state cyclic stress and strain based on basic mechanical parameters in the technical field of mechanical fatigue strength. The invention can be used to model the cyclic stress and strain in the tension-torsion steady state, and the modeling results can be used for fatigue life prediction, safety performance evaluation and the like of engineering structures. Background technique [0002] In engineering practice, most machinery and engineering structures work under complex multiaxial stress states. Therefore, multiaxial fatigue failure is a common failure form of mechanical and structural parts, accounting for about 50% to 90% of mechanical failures. Since multiaxial fatigue failure usually has no obvious macroscopic plastic deformation, sudden fracture often occurs, causing great harm and economic loss. Compared with uniaxial fa...

Claims

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Application Information

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IPC IPC(8): G01N3/08G01N3/22G01N3/32G01N3/24
CPCG01N3/08G01N3/22G01N3/24G01N3/32G01N2203/0017G01N2203/0021G01N2203/0025G01N2203/0026G01N2203/0073G01N2203/0075
Inventor 李静仇原鹰白金王海东王肇喜
Owner XIDIAN UNIV
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