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空天防御  2024, Vol. 7 Issue (6): 112-119    
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热处理对贮箱用原位自生铝基复合材料组织和性能的影响
王磊1, 陈哲1,2, 王浩伟1,2
1. 上海交通大学 材料科学与工程学院特种材料研究所,上海 200240; 2. 上海交通大学 金属基复合材料国家重点实验室,上海 200240
Effect of Heat Treatment on Microstructure and Mechanical Properties of In-Situ Al Matrix Composite for Storage Tanks
WANG Lei1, CHEN Zhe1,2, WANG Haowei1,2
1. School of Materials Science and Engineering, Institute of special materials, Shanghai Jiao Tong University, Shanghai 200240, China; 2. State Key Laboratory of Metal Matrix Composites, Shanghai Jiao Tong University, Shanghai 200240, China
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摘要 为满足新一代航天器的轻量化需求,如何获得贮箱用原位自生TiB2/2219 复合材料最优的热处理工艺参数组合,以进一步提升其综合力学性能,成为急需解决的重要问题。本文通过先进的表征技术和室温力学性能数据分析,系统研究固溶时效工艺对原位TiB2/2219 复合材料力学性能的影响规律。结果表明:复合材料在535 ℃、1.5 h固溶条件下具有最高硬度,为108 HV;利用预拉伸使位错密度增加,为θ′相提供更多形核位点,提高了形核率,并增加时效过程中析出相的体积分数;设计中低温双级时效制度以促进原子团簇形成、增加析出相的形核位点,进一步提高θ′相的形核效率;在进行100 ℃×8 h 和160 ℃×13 h 时效后,屈服强度和抗拉强度相比未进行预拉伸的复合材料分别提高40.5% 和12.5%,且仍保持8.0% 的断裂应变。研究结果为我国航天贮箱用原位自生铝基复合材料的工程应用积累了有效的实验数据储备并提供技术支撑。
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关键词 铝基复合材料原位自生TiB2热处理工艺微观组织力学性能    
Abstract:To meet the lightweight requirements of the new generation of aerospace, obtaining the optimal heat treatment process parameter combination of in-situ TiB2/2219 composite for storage tanks to improve its comprehensive mechanical properties further has become an urgent problem. In this study, the effect of solution and ageing process on tensile properties of in-situ TiB2/2219 composite was systematically studied through advanced characterization techniques and analysis of tensile test data at room temperature was conducted. The results show that the compositehas the highest hardness of 108 HV at 535 ℃, 1.5 h solution. Pre-stretch can increase the dislocation density, provide more nucleation sites for θ' phase, improve the nucleation rate, and increase the volume fraction of the precipitated phase during ageing. To promote the formation of atomic clusters, increase the nucleation site of the precipitated phase, and further improve the nucleation efficiency of θ' phase, a two-stage ageing system was designed. After ageing at 100 ℃× 8 h and 160 ℃ ×13 h, the yield strength and tensile strength of the composite increased by 40.5% and 12.5%, respectively, while the fracture strain remained 8.0%. The results have accumulated effective experimental data and thus support the engineering application of in-situ aluminum matrix composites for space storage tanks.
Key wordsaluminum matrix composite    in-situ TiB2    heat treatment    microstructure    mechanical property
收稿日期: 2024-07-29      出版日期: 2025-01-16
ZTFLH:  TB 33  
基金资助:国家自然科学基金面上项目(51971137,52371034);上海交通大学新进青年教师启动计划(22X010500305)
作者简介: 王磊(1988—),男,博士,助理研究员。
引用本文:   
王磊, 陈哲, 王浩伟. 热处理对贮箱用原位自生铝基复合材料组织和性能的影响[J]. 空天防御, 2024, 7(6): 112-119.
WANG Lei, CHEN Zhe, WANG Haowei. Effect of Heat Treatment on Microstructure and Mechanical Properties of In-Situ Al Matrix Composite for Storage Tanks. Air & Space Defense, 2024, 7(6): 112-119.
链接本文:  
https://www.qk.sjtu.edu.cn/ktfy/CN/      或      https://www.qk.sjtu.edu.cn/ktfy/CN/Y2024/V7/I6/112

参考文献
[1] 李志强, 许斌, 林楠, 王一冲, 范根莲, 谭占秋, 张荻. 高模量高强韧碳纳米管/铝合金复合材料研究进展[J]. 空天防御, 2024, 7(6): 29-37.
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