Microstructure and Mechanical Properties of Core-Shell B4C-Reinforced Ti Matrix Composites

Author:

Xiu Ziyang1,Ju Boyu1ORCID,Zhan Junhai2,Zhang Ningbo3,Wang Pengjun4,Zhao Keguang5,Liu Mingda6,Yin Aiping2,Chen Weidi2,Jiao Yang2,Wang Hao2,Li Shuyang2,Zhu Xiaolin2,Wu Ping78,Yang Wenshu1ORCID

Affiliation:

1. State Key Laboratory of Advanced Welding and Jointing, Harbin Institute of Technology, Harbin 150001, China

2. Shanghai Aerospace System Engineering Research Institute, Shanghai 201108, China

3. Aerospace Research Institute of Materials & Processing Technology, Beijing 100076, China

4. Xi’an Honor Device Co., Ltd., Xi’an 710000, China

5. Huazhong Institute of Electro-Optics, Wuhan 430074, China

6. CASIC Space Engineering Development Co., Ltd., Xinzhou 431400, China

7. Key Laboratory of Advanced Science and Technology on High Power Microwave, Xi’an 710024, China

8. Northwest Institute of Nuclear Technology, Xi’an 710024, China

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.

Funder

National Key Research and Development Program of China

National Natural Science Foundation of China

Excellent Youth Scholars Project of Natural Science Foundation of Heilongjiang Province

Heilongjiang Touyan Team Program

Publisher

MDPI AG

Subject

General Materials Science

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