A creep model based on normalized parameters

王延荣; 程域钊; 李宏新; 刘香; 田爱梅

doi:10.13224/j.cnki.jasp.2017.03.021

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A creep model based on normalized parameters

更新时间：2026-07-07

- A creep model based on normalized parameters
- Vol. 32, Issue 3, Pages: 683-688(2017)
- 作者机构：
  
  1. 北京航空航天大学能源与动力工程学院,北京,100191
  2. 先进航空发动机协同创新中心,北京,100191
  3. 北京航空航天大学宇航学院,北京,100191
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.2017.03.021
  CLC：
- Published：2017
- 稿件说明：
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王延荣, 程域钊, 李宏新, 刘香, 田爱梅. 一种基于归一化参数的蠕变模型[J]. 航空动力学报, 2017, 32(3): 683-688.

doi: 10.13224/j.cnki.jasp.2017.03.021
王延荣, 程域钊, 李宏新, 刘香, 田爱梅. 一种基于归一化参数的蠕变模型[J]. 航空动力学报, 2017, 32(3): 683-688. DOI： 10.13224/j.cnki.jasp.2017.03.021.

doi: 10.13224/j.cnki.jasp.2017.03.021 DOI：

摘要

针对传统蠕变模型(如Norton律)不能模拟蠕变第3阶段的不足

提出了一种基于归一化参数的蠕变模型

该模型以归一化时间为变量

以归一化应力和归一化温度为参数

可完整描述蠕变曲线的所有3个阶段.在该模型的基础上提出了能更好地描述蠕变曲线第1阶段的改进形式.利用所发展的模型对直接时效GH4169G材料的蠕变试验曲线3个阶段进行了较好地模拟

验证了该模型的描述蠕变变形的能力；同时确立了所发展模型中各参数与归一化温度和归一化应力之间的函数关系

取得了较好的效果；并且能与有限元软件结合

表明所发展的模型可应用于实际结构的蠕变分析.

Abstract

In view of the deficiency that the traditional creep models

e.g. the Nortons law

cannot be used to simulate the third stage of creep

a creep model based on normalized time as a variable and the normalized stress and normalized temperature as parameters was presented. The developed model could describe all three stages of the creep curves. On the basis of the developed model

an improved model was put forward to describe the first stage of the creep curves better. Then feasibility of the developed model was validated by use of the experimental data of the direct aged GH4169G.The relationship between the parameters of the developed model and the dimensionless temperature，dimensionless stress was established. And the models can be used in finite element software

showing that the model can be applied to simulate the creep behavior of realistic structure.

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Related Author

HU Dianyin

LI Wenzhu

LIU Hui

JIN Shengzhe

程域钊

王延荣

ZHANG Li

HUANG Xin-yue

Related Institution

Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation, Beijing Institute of Aeronautical Materials, Aviation Industry Corporation of China

National Key Laboratory of Science and Technology on Advanced High Temperature Structure Materials, Beijing Institute of Aeronautical Materials, Aviation Industry Corporation of China

State Key Laboratory for Advanced Metals and Materials, University of Science and Technology Beijing

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