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真空压力浸渗制备CF/Al复合材料热收缩与残余应力数值模拟与实验研究
引用本文:张益豪,严毅,王振军,蔡长春,徐志锋,余欢.真空压力浸渗制备CF/Al复合材料热收缩与残余应力数值模拟与实验研究[J].稀有金属材料与工程,2022,51(2):661-668.
作者姓名:张益豪  严毅  王振军  蔡长春  徐志锋  余欢
作者单位:南昌航空大学,南昌航空大学,南昌航空大学,南昌航空大学,南昌航空大学,南昌航空大学
基金项目:国家自然科学基金资助(项目号51765045);航空科学基金资助(项目号2019ZF056013);江西省自然科学基金资助(项目号20202ACBL204010)
摘    要:针对连续碳纤维增强铝基复合材料(CF/Al复合材料),采用细观力学数值模拟与热性能试验结合的方法,研究了真空压力浸渗制备过程中的热收缩行为和热残余应力分布。结果表明,复合材料的横向热收缩应变量远大于轴向热收缩应变量,且具有横观各向同性,纤维随机分布的单胞有限元模型能够准确地预测复合材料轴向与横向热收缩行为曲线;复合材料制备完成后纤维和基体合金分别处于压应力和拉应力状态,基体和纤维的横向残余应力均小于其轴向残余应力,且均表现出横观各向同性;基体合金在轴向残余拉应力作用下会出现不同程度的损伤现象,特别是纤维间距较小部位过高的残余应力会引发界面的局部失效,从而不利于发挥复合材料承载性能,减少纤维局部偏聚是进一步改善提高复合材料力学性能的重要技术手段。

关 键 词:铝基复合材料  热残余应力  细观力学  热收缩  损伤
收稿时间:2021/2/20 0:00:00
修稿时间:2021/4/8 0:00:00

Numerical Simulation and Experimental Study on Thermal Shrinkage and Residual Stress of CF / Al Composite Prepared by Vacuum Pressure Infiltration
Zhang Yihao,Yan Yi,Wang Zhenjun,Cai Changchun,Xu Zhifeng and Yu Huan.Numerical Simulation and Experimental Study on Thermal Shrinkage and Residual Stress of CF / Al Composite Prepared by Vacuum Pressure Infiltration[J].Rare Metal Materials and Engineering,2022,51(2):661-668.
Authors:Zhang Yihao  Yan Yi  Wang Zhenjun  Cai Changchun  Xu Zhifeng and Yu Huan
Affiliation:School of Aeronautical Manufacturing Engineering,Nanchang Hangkong University,School of Materials Science and Engineering,Nanchang Hangkong University,School of Aeronautical Manufacturing Engineering,Nanchang Hangkong University,School of Aeronautical Manufacturing Engineering,Nanchang Hangkong University,School of Aeronautical Manufacturing Engineering,Nanchang Hangkong University,School of Aeronautical Manufacturing Engineering,Nanchang Hangkong University
Abstract:For continuous carbon fiber reinforced aluminum matrix composites (CF/Al composites), the thermal shrinkage behavior and thermal residual stress distribution in the vacuum pressure infiltration preparation process were studied by combining the numerical simulation with the thermal performance test. The results show that the transverse thermal shrinkage strain of the composite is much larger than that the axial thermal shrinkage strain, and it is transversely isotropic. The radom fiber arrangement RVE model can accurately predict the axial and transverse thermal shrinkage behavior curves of the composite. In the prepared composite, the fiber and matrix alloy are in compressive stress state and tensile stress state, respectively. The transverse residual stresses of the matrix alloy and fiber is less than their axial residual stresses, and both show the transverse isotropic. The matrix alloy will appear different degrees of damage under the action of axial residual tensile stress. Especially, the high residual stress at the small fiber spacing will cause local interfacial failure, which is not conducive to the bearing capacity of the composite. It is an important technical approach to reduce the local segregation of fibers in order to improve the mechanical properties of the composite.
Keywords:aluminum matrix composites  thermal residual stress  micromechanics  thermal shrinkage  Damage
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