首页 | 本学科首页   官方微博 | 高级检索  
     检索      

TiC 颗粒增强钛基复合材料的动态损伤本构
引用本文:李,伟.TiC 颗粒增强钛基复合材料的动态损伤本构[J].宇航材料工艺,2012,42(4):37-41.
作者姓名:  
作者单位:中国轻型燃气轮机开发中心,北京,100028
摘    要:分析了TiC颗粒增强钛基复合材料的微损伤演化规律,建立了含损伤演化的动态本构模型。TiC颗粒增强钛基复合材料在拉伸载荷作用下,微裂纹以翼型裂纹形式扩展,基于平面翼型裂纹扩展模型,建立了二维动态损伤本构关系,并退化到一维拉伸状态,假设微裂纹成核规律满足Weibull分布,得到了一维拉伸应力状态下能够反映TiC颗粒增强钛基复合材料的损伤演化规律的宏细观相结合的动态本构关系。模型计算结果与试验结果吻合较好。

关 键 词:钛基复合材料  TiC颗粒  动态  损伤演化  本构模型

Dynamic Damage Constitutive of TiC Particle Reinforced Titanium Matrix Composites
Li Wei.Dynamic Damage Constitutive of TiC Particle Reinforced Titanium Matrix Composites[J].Aerospace Materials & Technology,2012,42(4):37-41.
Authors:Li Wei
Institution:Li Wei(China Gas Turbine Development Center,Beijing 100028)
Abstract:The micro-damage evolution of TiC particle reinforced titanium matrix composites was analyzed, and
a dynamic constitutive model with damage evolution was established. When TiC particle reinforced titanium matrix
composites withstands tensile loads, micro-cracks expand in form of wing cracks through the matrix. Based on the
wing crack growth model, a biaxial damage evolution constitutive was set up. And by degenerating, the uniaxial tension
damage evolution constitutive was gotten. It is assumed that microcrack nucleation law accords with Weibull distribution,
then a macroscopic and microscopic combined dynamic constitutive model in a one-dimensional stress state
was established, which can reflect the damage evolution of TiC particle reinforced titanium matrix composites. Model
simulation results agree well with the experimental curves.
Keywords:Titanium matrix composites  TiC particles  Dynamic  Damage evolution  Constitutive model
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《宇航材料工艺》浏览原始摘要信息
点击此处可从《宇航材料工艺》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号