Hafnium boride (HfB2) ultra-high temperature ceramics have become one of the best candidate materials in the field of thermal protection due to their high melting point, high oxidation resistance and excellent corrosion resistance. The fabrication of ceramic powders with precisely controlled particle sizes is paramount for their effective application. Highpurity HfB2 ceramic powders were prepared by crystal seed-mediated boro/carbothermal reduction method using hafnium oxide (HfO2), boron trioxide (B2O3), and carbon (C) powders as raw materials. The influence of crystal seed size on the particle size of HfB2 powders was studied, and the growth mechanism of HfB2 powders synthesized by crystal seed-mediated method was explored. Phase and morphology of the obtained powders were analyzed and observed by X-ray diffraction and scanning electron microscope; the contents of C and O impurities in the powders were measured as well. The results show that the optimal reaction temperature for synthesizing pure HfB2 powders by crystal seed-mediated boro/carbothermal reduction is approximately 1500 ℃ (holding for 1 h). HfB2 ceramic powders with average particle size of 1.08–2.33 μm were obtained by controlling the initial crystal seed size. Generally, the particle size of HfB2 increases with the increase of crystal seed size, and laser particle size measurements indicate that the addition of crystal seeds improves the dispersibility and narrows distribution of HfB2 particle size. It is confirmed that the growth process of HfB2 ceramic powders is divided into two stages: the cladding of HfO2 grains on HfB2 surface with formation of tiny HfB2 grains, and conversion of HfO2 to HfB2 through mass diffusion of carbon and boron from the outside to the inside of HfO2 particles.
王振,胡晨光,李可为,胡梦恩,张瀚文,黄竹林,胡小晔. 晶种法合成硼化铪粉体及其生长机理研究[J]. 航空制造技术, 2025, 68(3): 84-91.
WANG Zhen, HU Chenguang, LI Kewei, HU Mengen, ZHANG Hanwen, HUANG Zhulin, HU Xiaoye. Synthesis and Growth Mechanism Research of HfB2 Powders Prepared by Crystal Seed-Mediated Method[J]. Aeronautical Manufacturing Technology, 2025, 68(3): 84-91.