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Prediction method for material multiaxial creep failure strain

A prediction method and prediction equation technology, applied in the field of strain prediction, can solve the problems of lack of physical meaning, unreasonable multi-axial creep failure strain prediction, etc., and achieve accurate prediction effect

Active Publication Date: 2017-07-07
CHINA UNIV OF PETROLEUM (EAST CHINA)
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Problems solved by technology

Although the multiaxial creep ductility factor can be easily used to model creep crack growth and give acceptable prediction results, it lacks due physical meaning, and in some cases, the Cocks-Ashby MCDF is more Prediction of shaft creep failure strain is unreasonable and needs improvement

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  • Prediction method for material multiaxial creep failure strain
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  • Prediction method for material multiaxial creep failure strain

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Embodiment Construction

[0035] Figure 1~7 It is the best embodiment of the present invention, below in conjunction with attached Figure 1~7 The present invention will be further described.

[0036] Such as figure 1 As shown, a material multiaxial creep failure strain prediction method is characterized in that: comprising the following steps:

[0037] Step (1), based on the strain damage criterion, according to the microscopic pore growth mechanism, the relationship between the material creep rate and the strain rate is obtained;

[0038] The microscopic pore growth mechanism considers that pores are mainly nucleated and grown on the grain interface (especially on the grain interface perpendicular to the tensile stress), and the fully grown pores will aggregate to form microcracks of grain size (porosity grain size). interface). Finally, the coalescence of microcracks leads to the propagation of macroscopic creep cracks.

[0039] Although vacancy condensation, grain boundary slip, and dislocati...

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Abstract

The invention discloses a prediction method for material multiaxial creep failure strain, and belongs to the technical field of strain prediction. The prediction method is characterized in comprising the following steps that: S(1): obtaining a relationship between a material creep rate and a strain rate; S(2): controlling a cavity growth theory by power-law creep, and obtaining single-axis and multi-axis strain state parameters; S (3): expressing the creep failure strain under single-axis and multi-axis strain functions, and obtaining a multi-axis creep ductility factor; S(4): obtaining a multiaxial creep failure strain fitting parameter under different strain states so as to obtain a multiaxial creep failure ductility factor prediction equation; and S(5): utilizing finite element software to predict the creep failure strain and the service life of the material under the multi-axis strain state. By use of the prediction method for the material multiaxial creep failure strain, through a creep failure strain calculation method of the material under the multi-axis strain state, the multiaxial creep failure strain of the material under a high-temperature state can be more accurately predicted.

Description

technical field [0001] The invention discloses a material multiaxial creep failure strain prediction method, which belongs to the technical field of strain prediction. Background technique [0002] In the fields of nuclear power, petrochemical and aerospace, many structural components such as heat exchangers work under high temperature and high pressure for a long time, and the entire structure is in a complex multiaxial stress state. Creep and the damage caused by it are the main failure modes of the structure one. Creep-damage failure research under multiaxial stress state is one of the most important links in structural integrity assessment. The forecast is positive. [0003] Aiming at the problem of complicated model parameters, the strain-based continuum damage mechanics model has been paid more and more attention. The model based on strain damage is also called the ductility depletion model. It is believed that when the local creep strain accumulation reaches the cr...

Claims

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Application Information

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IPC IPC(8): G06F17/50
CPCG06F30/17G06F30/23G06F2119/06
Inventor 张玉财蒋文春王传龙涂善东王宁
Owner CHINA UNIV OF PETROLEUM (EAST CHINA)