A multi-axis creep fatigue prediction method based on ABAQUS

A prediction method and creep technology, applied in the direction of using stable tension/pressure to test material strength, measurement device, knowledge expression, etc., can solve the problems of inaccurate creep fatigue analysis and prediction, poor convergence, complex programming, etc.

Active Publication Date: 2019-06-14
EAST CHINA UNIV OF SCI & TECH
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Problems solved by technology

However, these three types of methods have their own shortcomings: the first type of method is only suitable for describing the stress-strain behavior at the microscopic level, and is not suitable for large high-temperature components at the macroscopic level; the second type of method focuses on describing the creep fatigue in the crack growth stage Behavior, its complex programming, poor convergence, high computational cost and other characteristics determine that this type of method does not have strong universality; although the third type of method has the characteristics of strong operability, it is mostly used to analyze single-axis in a steady state. Stress-strain behavior, not accurate for creep fatigue analysis and prediction under complex stress-strain state and complex loading history

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  • A multi-axis creep fatigue prediction method based on ABAQUS
  • A multi-axis creep fatigue prediction method based on ABAQUS
  • A multi-axis creep fatigue prediction method based on ABAQUS

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Embodiment Construction

[0066] The ABAQUS-based multiaxial creep fatigue prediction method of the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0067] figure 1 It is a flow chart of the ABAQUS-based multiaxial creep fatigue prediction method in one embodiment of the present invention.

[0068] Such as figure 1 As shown, in this embodiment, the ABAQUS-based multiaxial creep fatigue prediction method includes steps:

[0069] S1: Establish the ABAQUS finite element model, and define the viscoplastic constitutive equation of the material to be tested in the process of cyclic loading through the user subroutine UMAT;

[0070] S2: determining the model parameters required by the viscoplastic constitutive equation;

[0071] S3: Establish a fatigue damage calculation model and a creep damage calculation model of the multiaxial stress-strain state of the material to be tested;

[0072] S4: Establish the ABAQUS finite e...

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Abstract

The invention discloses a multi-axis creep fatigue prediction method based on ABAQUS, and the method comprises the steps of S1, building an ABAQUS finite element model, and defining a viscoplastic constitutive equation of a to-be-tested material through a user subprogram UMAT; S2, determining model parameters required by the viscoplastic constitutive equation; S3, establishing a fatigue damage calculation model and a creep damage calculation model of the multi-axis stress-strain state of the to-be-tested material; S4, establishing an ABAQUS finite element model in a multi-axis stress-strain state, and calculating to obtain a stress-strain tensor of each cycle on the basis of the defined viscoplastic constitutive equation and model parameters; and S5, calculating equivalent stress and equivalent plastic strain through a user subprogram USDFLD, and superposing fatigue damage and creep damage of each cycle through a linear cumulative damage criterion on the basis of the fatigue damage calculation model and the creep damage calculation model in combination with the stress strain tensor to obtain the crack initiation life.

Description

technical field [0001] The invention relates to the field of numerical simulation, in particular to a multi-axis creep fatigue prediction method. Background technique [0002] With the increasing demand for large-scale, high-performance, and long-life high-temperature rotating parts, the structural integrity assessment of structures containing geometric discontinuities in complex and harsh environments has become one of the key technical bottlenecks that need to be solved urgently. The multiaxial stress-strain regimes resulting from geometric discontinuities and complex loading histories inevitably become the limiting service life of such components. In recent years, the development of finite element software can satisfy people's understanding of complex stress-strain behavior and provide the feasibility of accurate life prediction in this state. [0003] Nowadays, creep fatigue analysis and life prediction of complex structures can be mainly divided into three categories. ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F17/00G01N2203/0214G06N20/00G06F30/23G06F2119/04G06F2119/14G01N3/08G01N2203/0071G01N2203/0073G06N5/02
Inventor 王润梓张显程郭素娟苑光健朱旭旻涂善东
Owner EAST CHINA UNIV OF SCI & TECH
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