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Publishing Language: Chinese

Research progress on refractory metal and metallic carbide/oxide powder preparation techniques

Yupeng WEI1,2,3, Shan CHEN1,2, Yating WANG1,2, Dongxin WANG3, Yanhong YU1,2, Meng ZHANG1,2, Rongzhen XIAO1,2( ), Liang ZHU1,2, Yuewei CHENG3
School of Materials Science and Engineering, Lanzhou University of Technology, Lanzhou 730050, China
State Key Laboratory of Advanced Processing and Recycling of Nonferrous Metals, Lanzhou University of Technology, Lanzhou 730050, China
Northwest Rare Metal Materials Research Institute Ningxia Co., Ltd, Shizuishan 753000, China
State Key Laboratory of Special Rare Metal Materials, Shizuishan 753000, China
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Abstract

Having such excellent properties as high melting point, high temperature stability, and strong corrosion resistance, refractory metals, metallic carbides and metallic oxides. These are widely used in high-temperature and high-pressure, strong corrosion and other environments such as gas blades, electronic tubes, rocket engines, cutting tools, high temperature thermal components, and turbine nozzles. Focusing on the preparation methods of refractory metals and metallic carbides/oxides powder, including the mechanical method, reduction method, combustion method, sol-gel method, hydrothermal method, microwave method, precipitation method, pyrolysis method, explosion method and plasma method, this paper analyzed the advantages, disadvantages and status of preparation methods such as Mo, W, Ta, WC, ZrC, TiC, CeO2, ZrO2 and Y2O3, and prospected the development status of the preparation of refractory powder based on electric explosion method to provide reference for the preparation and application of refractory powders.

CLC number: V19; TB35 Document code: A

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Acta Aeronautica et Astronautica Sinica
Article number: 028719

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Cite this article:
WEI Y, CHEN S, WANG Y, et al. Research progress on refractory metal and metallic carbide/oxide powder preparation techniques. Acta Aeronautica et Astronautica Sinica, 2024, 45(3): 028719. https://doi.org/10.7527/S1000-6893.2023.28719

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Received: 20 March 2023
Revised: 16 May 2023
Accepted: 05 June 2023
Published: 19 June 2023
© 2024 The Journal of Acta Aeronautica et Astronautica Sinica