首页|航天用碳纳米管增强铝合金复合材料的力学与阻尼性能

航天用碳纳米管增强铝合金复合材料的力学与阻尼性能

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碳纳米管(CNT)作为增强体的铝基复合材料(CNT/Al)具有轻质、高强、高模量、易加工的性能优势,用作轻量化材料在航天航空领域具有巨大的应用前景.为了获得兼顾其力学性能和阻尼性能的轻量化结构材料,采用叠片粉末冶金与合金化方法制备了质量分数为1.5%CNT/2A12复合材料,并研究了不同时效条件下的力学性能与阻尼性能.在130℃时效6~14 h时,复合材料具有最佳的拉伸强度与延伸率,抗拉强度最高可达595 MPa(时效12 h),延伸率最高可达14.0%(时效8 h).复合材料的阻尼在0~180℃时变化不大,其在0.005左右,180~300℃时明显提高,300℃时可达0.05,阻尼性能受时效时间影响不大.复合材料的储存模量随测试温度升高而下降,在180~300℃时随振动频率升高而升高.时效条件为130℃-8 h时,质量分数1.5%CNT/2A12复合材料性能兼具良好的力学性能与阻尼性能.
Mechanical Properties and Damping Capacity of CNT Reinforced Aluminum Maxtrix Composites
Carbon nanotube(CNT)reinforced aluminum matrix(CNT/Al)composites have the advantages of light weight,high strength,high modulus,and easy processing,and have a great application prospect in the aerospace field as lightweight materials.In order to obtain a lightweight structural material with both good mechanical properties and perfect damping capacity,the 1.5%(mass fraction)CNT/2A12 composite is prepared by flake powder metallurgy and elemental alloying.When the composite is aged at 130℃for 6~14 h,it exhibits high tensile strength and good ductility.The tensile strength is up to 595 MPa at 12 h of aging,and the elongation is up to 14.0%at 8 h of aging.The damping capacity of the composite is about 0.005 at 0~180℃,but significantly increases at 180~300℃,reaching 0.05 at 300℃.The damping capacity is hardly affected by the aging time.The storage modulus of the composite decreases when the test temperature increases,and increases at 180~300℃when the vibration frequency increases.Taking the overall properties into consideration,at 130℃and 8 h,the 1.5%(mass fraction)CNT/2A12 composite has the optimal mechanical properties and damping capacity.

CNT/Al compositeheat treatmentmechanical propertydamping capacitystorage modulus

黄静宏、邹仁珍、陈航、朱帅、江燕、范根莲、谭占秋、李志强、张荻

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上海交通大学 金属基复合材料国家重点实验室 材料科学与工程学院,上海 200240

上海机电工程研究所,上海 201109

上海航天设备制造总厂有限公司,上海 200245

CNT/2A12复合材料 热处理 力学性能 阻尼性能 储存模量

国家自然科学基金国家自然科学基金国家自然科学基金中国航天科技集团公司第八研究院产学研合作基金

521711435219259252192595USCAST2022-01

2024

上海航天(中英文)
上海航天技术研究院

上海航天(中英文)

CSTPCD
影响因子:0.166
ISSN:2096-8655
年,卷(期):2024.41(3)