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3D-Cf / Mg 复合材料的热残余应力研究
引用本文:谢薇.3D-Cf / Mg 复合材料的热残余应力研究[J].宇航材料工艺,2012,42(3):75-77,85.
作者姓名:谢薇
作者单位:上海交通大学材料科学与工程学院,航空航天新材料研究中心,上海 200240
摘    要:采用随动硬化有限元模型,研究了三维碳纤维增强镁基复合材料(3D-Cf/Mg)基体热残余应力的大小、分布以及不同工艺处理对热残余应力的影响。同时,对复合材料进行了高、低温处理,利用XRD定性分析了处理前后复合材料基体热残余应力的变化。计算结果表明:经过-196℃低温处理后,复合材料基体的平均Mises热残余应力由169.06 MPa减小至55.29 MPa;高温处理后,基体平均热残余应力几乎不变。该结果与实验结果吻合,证明了低温处理能明显降低复合材料基体的热残余应力。

关 键 词:三维碳纤维  镁基复合材料  热残余应力  有限元

Thermal Residual Stress in 3D-Cf / Mg
Xie Wei , Zhou Cong , Ma Naiheng , Wang Haowei.Thermal Residual Stress in 3D-Cf / Mg[J].Aerospace Materials & Technology,2012,42(3):75-77,85.
Authors:Xie Wei  Zhou Cong  Ma Naiheng  Wang Haowei
Institution:Xie Wei Zhou Cong Ma Naiheng Wang Haowei(Advanced Material Center of Aeronautics & Aerospace,School of Materials Science and Engineering,Shanghai Jiaotong University,Shanghai 200240)
Abstract:This paper proposes a nonlinear elastoplastic model and uses the finite element method to study the thermal residual stress in 3D-Cf/Mg and its modification after different treatments.Then an experimental investigation was realized by XRD,which indicates the influences of different treatments on thermal residual stress.The result shows that after a cold-treatment at-196℃,the average thermal residual stress can decrease from 169.06 MPa to 55.29 MPa,while the thermal residual stress changes little after a heat-treatment.This calculating result agrees well with the experimental results and proves that the cold-treatment can reduce the thermal residual stress in 3D-Cf/Mg.
Keywords:3D woven carbon fiber  Mg composite  Thermal residual stress  Finite elements
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