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高Nb-TiAl合金高温力学行为本构建模仿真技术

董成利 于慧臣 焦泽辉 孔凡涛 陈玉勇

航空材料学报2018,Vol.38Issue(1):80-87,8.
航空材料学报2018,Vol.38Issue(1):80-87,8.DOI:10.11868/j.issn.1005-5053.2017.000070

高Nb-TiAl合金高温力学行为本构建模仿真技术

High Temperature Mechanical Constitutive Modeling of a High-Nb TiAl Alloy

董成利 1于慧臣 2焦泽辉 3孔凡涛 1陈玉勇2

作者信息

  • 1. 中国航发北京航空材料研究院先进高温结构材料重点实验室,北京100095
  • 2. 航空材料检测与评价北京市重点实验室,北京100095
  • 3. 材料检测与评价航空科技重点实验室,北京100095
  • 折叠

摘要

Abstract

Uniaxial tensile,low cycle fatigue,fatigue-creep interaction and creep experiments of a novel high-Nb TiAl alloy (i. e. Ti-45Al-8Nb-0. 2W-0. 2B-0. 02Y (atom fraction/%))were conducted at 750 ℃ to obtain its tested data and curves. Based on Chaboche visco-plasticity unified constitutive model,Ohno-Wang modified non-linear kinematic hardening was introduced in Chaboche constitu-tive model to describe the cyclic hardening/softening,and Kachanov damage was coupled in Chaboche constitutive model to character-ize the accelerated creep stage. The differential equations of the constitutive model discretized by explicit Euler method were compiled in to ABAQUS/UMAT to simulate the mechanical behavior of high-Nb TiAl alloy at different test conditions. The results show that Chaboche visco-plasticity unified constitutive model considering both Ohno-Wang modified non-linear kinematic hardening and Kacha-nov damage is able to simulate the uniaxial tensile,low cycle fatigue,fatigue-creep interaction and creep behavior of high-Nb TiAl alloy and has high accuracy.

关键词

高Nb-TiAl合金/低周疲劳/疲劳-蠕变交互/蠕变/本构模型

Key words

high-Nb TiAl alloy/low cycle fatigue (LCF)/fatigue-creep interaction/creep/constitutive model

分类

矿业与冶金

引用本文复制引用

董成利,于慧臣,焦泽辉,孔凡涛,陈玉勇..高Nb-TiAl合金高温力学行为本构建模仿真技术[J].航空材料学报,2018,38(1):80-87,8.

基金项目

国家自然科学基金-青年基金项目(51401195 ) (51401195 )

国家重点基础研究发展计划(973计划)(2011CB605501) (973计划)

航空基金项目(2013ZF21014) (2013ZF21014)

航空材料学报

OA北大核心CSCDCSTPCD

1005-5053

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