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Open Access

Micro powder injection molding of boron carbide components with SiC-Al2O3-Y2O3 sintering additives

Changrui WANGaZhiyou LIaWei TIANa( )Yuxian LIbLina TANGcQilong PANGdMinghe CHENa
National Key Laboratory of Science and Technology on Helicopter Transmission, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Ji’nan Technician College, Jinan 250000, China
Shanghai Aerospace Equipments Manufacturer Co. Ltd., Shanghai 200245, China
College of Mechanical and Electrical Engineering, Nanjing Forestry University, Nanjing 210037, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Sintering additives and micro-powder injection molding offer an effective method to densify boron carbide (B4C) and make B4C components with complex shapes. By adjusting the proportion of three kinds of powders (SiC, Al2O3 and Y2O3), four kinds of sintering additives were prepared. The feedstock uniformity, debinding behavior, phase composition and microstructure of micro injection molded B4C components with different sintering additives were studied. The results showed that the defects such as lattice distortion and vacancy were introduced into ball milling, which increase the surface energy and benefit subsequent sintering densification. The feedstock had good uniformity and rheology that met the requirements of micro powder injection molding. After debinding, B4C components had enough strength and showed certain sintering characteristics. The addition of sintering additives was beneficial to densification and sintering temperature reduction. The addition of sintering additives formed a second phase in the B4C crystal and at the grain boundary of B4C crystal, which changed the fracture mode from transgranular fracture to mixed fracture mechanism with transgranular fracture.

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Chinese Journal of Aeronautics
Pages 429-440

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Cite this article:
WANG C, LI Z, TIAN W, et al. Micro powder injection molding of boron carbide components with SiC-Al2O3-Y2O3 sintering additives. Chinese Journal of Aeronautics, 2022, 35(5): 429-440. https://doi.org/10.1016/j.cja.2020.08.005

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Received: 12 April 2020
Revised: 29 April 2020
Accepted: 07 May 2020
Published: 17 August 2020
© 2021 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).