马广义

个人信息Personal Information

教授

博士生导师

硕士生导师

主要任职:机械工程学院副院长

性别:男

毕业院校:大连理工大学

学位:博士

所在单位:机械工程学院

学科:机械制造及其自动化. 机械电子工程. 机械设计及理论

办公地点:机械知方楼5035

联系方式:0411-84706920

电子邮箱:gyma@dlut.edu.cn

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High-mass-proportion TiCp/Ti6Al4V titanium matrix composites prepared by directed energy deposition

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论文类型:期刊论文

发表时间:2021-01-10

发表刊物:ADDITIVE MANUFACTURING

卷号:35

ISSN号:2214-8604

关键字:Metal-matrix composites; Titanium matrix composites; Microstructure; Mechanical properties; Laser additive manufacturing

摘要:Titanium matrix composites (TMC) have potential applications in the aerospace industry because of their excellent performance. The comprehensive performance of TMC mainly depends on the matrix, reinforcement and interface characteristics. Hence, this study discussed the knowledge of microstructure-property relationships in detail. Crack-free high-mass-proportion TiCp/Ti6Al4Vcomposites were successfully prepared by directed energy deposition (DED). As the TiCp mass fraction increasing from 0 to 50%, the quantity of primary TiC and unmelted TiC (UMT) increased. Meanwhile, the refined alpha-Ti in the composites had a relatively weak texture. In addition, the interface between primary TiC and alpha-Ti was a semi-coherent interface, exhibiting a [11 (2) over bar0] alpha-Ti // [110]TiC, ((1) over bar 100) alpha-Ti // ((1) over bar 11) TiC orientation relationship, which facilitated the heterogeneous nucleation of Ti and improved bonding of primary TiC with the matrix. With the increase in microhardness taking the form of a cubic function, the wear mechanism was found to transform from abrasive wear to slight delamination wear. Due to the fact that both UMT and primary TiC bonded well with Ti64 matrix, they shared partial friction to protect matrix from severe abrasion, resulting in an excellent wear resistance of composites. Moreover, the thermal conductivity of 50% TiCp/Ti6Al4V was 9.063 W.m(-1) .K-1, which was nearly 26.5% higher than that of Ti6Al4V. Owing to the premature cracking of brittle UMT and dendritic TiC, the tensile strength and elongation of the composite with 50% TiCp were 515.5 MPa and 1.83%, which decreased by 45.8% and 78.8%, respectively. Adding a high proportion of TiCp can significantly improve the hardness and wear resistance of TMC, whereas it is detrimental to the tensile performance of TMC. The study have significant implications for the design of novel TMC, particularly for the aerospace industrial applications.