Microstructure and Mechanical Properties of Core-Shell B4C-Reinforced Ti Matrix Composites
Composite material uses ceramic reinforcement to add to the metal matrix to obtain higher material properties. Structural design is an important direction of composite research. The reinforcement distribution of the core-shell structure has the unique advantages of strong continuity and uniform stre...
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Published in | Materials Vol. 16; no. 3; p. 1166 |
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Main Authors | , , , , , , , , , , , , , , |
Format | Journal Article |
Language | English |
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Abstract | Composite material uses ceramic reinforcement to add to the metal matrix to obtain higher material properties. Structural design is an important direction of composite research. The reinforcement distribution of the core-shell structure has the unique advantages of strong continuity and uniform stress distribution. In this paper, a method of preparing boron carbide (B4C)-coated titanium (Ti) powder particles by ball milling and preparing core-shell B4C-reinforced Ti matrix composites by Spark Plasma Sintering was proposed. It can be seen that B4C coated on the surface of the spherical Ti powder to form a shell structure, and B4C had a certain continuity. Through X-ray diffraction characterization, it was found that B4C reacted with Ti to form layered phases of titanium boride (TiB) and titanium carbide (TiC). The compressive strength of the composite reached 1529.1 MPa, while maintaining a compressive strain rate of 5%. At the same time, conductivity and thermal conductivity were also characterized. The preparation process of the core-shell structure composites proposed in this paper has high feasibility and universality, and it is expected to be applied to other ceramic reinforcements. This result provides a reference for the design, preparation and performance research of core-shell composite materials. |
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AbstractList | Composite material uses ceramic reinforcement to add to the metal matrix to obtain higher material properties. Structural design is an important direction of composite research. The reinforcement distribution of the core-shell structure has the unique advantages of strong continuity and uniform stress distribution. In this paper, a method of preparing boron carbide (B
4
C)-coated titanium (Ti) powder particles by ball milling and preparing core-shell B
4
C-reinforced Ti matrix composites by Spark Plasma Sintering was proposed. It can be seen that B
4
C coated on the surface of the spherical Ti powder to form a shell structure, and B
4
C had a certain continuity. Through X-ray diffraction characterization, it was found that B
4
C reacted with Ti to form layered phases of titanium boride (TiB) and titanium carbide (TiC). The compressive strength of the composite reached 1529.1 MPa, while maintaining a compressive strain rate of 5%. At the same time, conductivity and thermal conductivity were also characterized. The preparation process of the core-shell structure composites proposed in this paper has high feasibility and universality, and it is expected to be applied to other ceramic reinforcements. This result provides a reference for the design, preparation and performance research of core-shell composite materials. Composite material uses ceramic reinforcement to add to the metal matrix to obtain higher material properties. Structural design is an important direction of composite research. The reinforcement distribution of the core-shell structure has the unique advantages of strong continuity and uniform stress distribution. In this paper, a method of preparing boron carbide (B4C)-coated titanium (Ti) powder particles by ball milling and preparing core-shell B4C-reinforced Ti matrix composites by Spark Plasma Sintering was proposed. It can be seen that B4C coated on the surface of the spherical Ti powder to form a shell structure, and B4C had a certain continuity. Through X-ray diffraction characterization, it was found that B4C reacted with Ti to form layered phases of titanium boride (TiB) and titanium carbide (TiC). The compressive strength of the composite reached 1529.1 MPa, while maintaining a compressive strain rate of 5%. At the same time, conductivity and thermal conductivity were also characterized. The preparation process of the core-shell structure composites proposed in this paper has high feasibility and universality, and it is expected to be applied to other ceramic reinforcements. This result provides a reference for the design, preparation and performance research of core-shell composite materials. |
Author | Yang, Wenshu Zhan, Junhai Li, Shuyang Wang, Pengjun Zhu, Xiaolin Chen, Weidi Yin, Aiping Zhang, Ningbo Ju, Boyu Zhao, Keguang Jiao, Yang Liu, Mingda Wu, Ping Xiu, Ziyang Wang, Hao |
AuthorAffiliation | 5 Huazhong Institute of Electro-Optics, Wuhan 430074, China 3 Aerospace Research Institute of Materials & Processing Technology, Beijing 100076, China 1 State Key Laboratory of Advanced Welding and Jointing, Harbin Institute of Technology, Harbin 150001, China 6 CASIC Space Engineering Development Co., Ltd., Xinzhou 431400, China 8 Northwest Institute of Nuclear Technology, Xi’an 710024, China 4 Xi’an Honor Device Co., Ltd., Xi’an 710000, China 7 Key Laboratory of Advanced Science and Technology on High Power Microwave, Xi’an 710024, China 2 Shanghai Aerospace System Engineering Research Institute, Shanghai 201108, China |
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SubjectTerms | B4C Ball milling Boron carbide Ceramic matrix composites Composite materials Compressive properties Compressive strength Continuity core-shell composite Core-shell structure High temperature Hot pressing Material properties Mechanical properties Metal matrix composites Morphology Particle size Plasma sintering R&D Research & development Sintering (powder metallurgy) Spark plasma sintering Spherical powders Strain rate Stress distribution Structural design Thermal conductivity Ti matrix composite Titanium alloys Titanium carbide Titanium diboride |
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Title | Microstructure and Mechanical Properties of Core-Shell B4C-Reinforced Ti Matrix Composites |
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