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High-Temperature Thermal Shock Performance of Si-Ti-Cr Silicide Coating on Nb-Hf Alloy Surface in Atmosphere and Vacuum
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1.Beijing Xinghang Mechanical-Electrical Equipment Co., Ltd, Beijing 100074, China;2.School of Instrumentation Science and Engineering, Harbin Institute of Technology, Harbin 150001, China;3.Institute for Advanced Ceramics, Harbin Institute of Technology, Harbin 150001, China

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National Defense Technical Basic Research Program of China (JSZL 2015603 B 002); Aviation Science Fund Project (20172777007); National Basic Science Research Program (52206225)

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    Abstract:

    To improve the high-temperature thermal shock performance, the Si-Ti-Cr silicide coatings were prepared on Nb-Hf alloy by slurry sintering and high-temperature permeation methods. The high-temperature thermal shock performance of Si-Ti-Cr silicide-coated Nb-Hf alloys in atmosphere and vacuum was comparatively analyzed. The failure mechanism of Si-Ti-Cr coating in atmosphere and vacuum after thermal shock tests was determined by simulating the temperature and thermal stress distributions of the coating during thermal shock. Results show that the mass loss of the coating in vacuum is less than 0.8 mg/cm2 after 100 thermal shock cycles at 1300 °C. The mass gain of the coating in atmosphere is less than 3 mg/cm2 after 200 thermal shock cycles at 1600 °C. Therefore, the silicide coating exhibits excellent thermal shock resistance at 1300 °C in vacuum and at 1600 °C in atmosphere.

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[An Dongyang, Liu Chenfei, Zhao Shuang, Zhang Haipeng, Tang Zengwu, Xiao Peng, Dai Jingmin, Wang Yaming. High-Temperature Thermal Shock Performance of Si-Ti-Cr Silicide Coating on Nb-Hf Alloy Surface in Atmosphere and Vacuum[J]. Rare Metal Materials and Engineering,2022,51(11):3974~3980.]
DOI:10.12442/j. issn.1002-185X.20220149

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History
  • Received:February 27,2022
  • Revised:August 09,2022
  • Adopted:August 24,2022
  • Online: December 07,2022
  • Published: November 30,2022