Investigating the Oxidation Resistance of HfCZrCTiC Composite at 1200 °C: The Role of Nano Carbon Black and Silicon

Document Type : Original Article

Authors

Department of Materials Science and Engineering, Ahvaz Branch, Islamic Azad University, Ahvaz, Iran

Abstract

Introduction and Objectives: The HfCZrCTiC composite is part of the family of ultra-high temperature ceramics used in heat shields for spacecraft, furnace linings, supersonic aircraft components, and nuclear reactor components. The purpose of this research is to investigate the effect of nanocarbon black and silicon on the oxidation resistance of HfCZrCTiC composite.
Materials and Methods: Four composites, including HfCZrCTiC, HfCZrCTiC containing nano carbon black, HfCZrCTiC containing silicon, and HfCZrCTiC containing nano carbon black and silicon simultaneously were sintered at 2000 °C by spark plasma method. The oxidation process was carried out using differential thermal analysis (DTA) and thermal gravimetry analysis (TGA) at a temperature of 1200 °C. Microstructural evaluation and phase identification were done using a scanning electron microscope and X-ray diffraction.
Results: The results showed that the weight changes for HfZrTi, HfZrTi-C.Bn, HfZrTi-Si and HfZrTi-C.Bn-Si samples were obtained to be 13.5%, 16.9%, 12.9%, and 7%, respectively. In addition, the results of differential thermal analysis (DTA) revealed that in the samples of HfZrTi, HfZrTi-C.Bn, HfZrTi-Si and HfZrTi-C.Bn-Si, the starting temperature of oxidation occurred at 480 °C, 400 °C, 500 °C, and 580 °C, respectively, indicating the lower the starting temperature of oxidation, the higher the weight changes.
Conclusion: It was found that in HfZrTi and HfZrTi-C.Bn samples, the detected phases after oxidation included hafnium oxide, zirconium oxide, and titanium oxide. These phases along with silicon oxide were identified in HfZrTi-Si and HfZrTi-C.Bn-Si samples.

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  1. Paul A, Jayaseelan DD, Venugopal S, Zapata-Solvas E, Binner JGP, Vaidhyanathan B, et al. UHTC Composites for Hypersonic Applications. Am Ceram Soc Bull. 2012;91(1):22-29.
  2. Wuchina E, Opeka M, Fahrenholtz WG, Talmy IG. UHTCs: Ultra-HighTemperature Ceramic Materials for Extreme Environment Applications. Scr Mater. 2007;16:112-143.
  3. Opeka M, Wuchina EJ, Zaykoski JA, Causey SJ. Mechanical, Thermal, and Oxidation Properties of Refractory Hafnium and zirconium Compounds. J Eur Ceram. 1999;19(13-14):2405-2414. https://doi. org/10.1016/S0955-2219(99)00129-6
  4. Shi X-H, Zhu J -L, Liu L, Li H-J, Hu X-J, Li M-Y, et al. Ablation resistance of SiC–ZrC coating prepared by a simple two-step method on carbon fiber reinforced composites. Corros Sci. 2014;88:49-55. https://doi.org/10.1016/j.corsci.2014.07.014
  5. Yan C, Zhang C, Cao Y, Wang Y. Effects of SiC/HfC ratios on the ablation and mechanical properties of 3D Cf/HfC-SiC composites. J Eur Ceram. 2017;37(6):2343-2351. https://doi.org/10.1016/j.jeurceramsoc.2017.01.017
  6. Xiang L, Fan X, Shi L, Yin X, Zhang L. Effect of interlayer on the ablation properties of laminated HfC–SiC ceramics under oxyacetylene torch. Corros Sci. 2015; 93:172-179. https://doi.org/10.1016/j.corsci.2015.01.021
  7. Fu YQ, Zhang J, Chen GH, Li T. Radially one-dimensional hafnium carbide-carbon/carbon networks composites for ultra-high temperature ablation-resistance. Corros Sci. 2021;185:109443. https://doi.org/10.1016/ j.corsci.2021.109443
  8. Jiachen L, Junshuai YZ, Tao L, Xiaofei Z, Gai W. Sealing role of Ti-rich phase in HfC-ZrC-TiC coating for C/C composites during ablation above 2100 °C. Corros Sci. 2022;205(15),110474. https://doi.org/10. 1016/j.corsci.2022.110474
  9. Chen Y, Xiang X, Chang YX, Peng Z, Tian T, Zeng Y. Microstructure, thermophysical properties, and ablation resistance of C/HfC-ZrC-SiC composites. Ceram Int. 2019;45(4):4685-4691. https://doi.org/10. 1016/j.ceramint.2018.11.160
  10. Balak Z, Zakeri M, Rahimipour MR, Salahi E, Azizieh M, Kafashan H. Investigation of effective parameters on densification of ZrB2-SiC based composites using taguchi method. Adv Ceram Prog. 2016;2(5):7-15. https://doi.org/10.30501/acp.2016.90835
  11. Malae Hezarvandi S, Balak Z, Heydari A. Fabrication and characterization of HfCZrCTiC composites: role of carbonaceous and metallic additives. J Korean Ceram Soc. 2024;61:1263–1277. https://doi.org/10.1007/s43207-024-00444-3
  12. Balak Z, Zakeri M. Effect of HfB2 on microstructure and mechanical properties of ZrB2-SiC-based composites. Int J Refract Met Hard Mater. 2016;54:127-135. https://doi.org/10.1016/j.ijrmhm.2015.07.011
  13. Balak Z, Azizieh M. Oxidation of ZrB2-SiC composites at 1600 °C: effect of carbides, borides, silicides, and chopped carbon fiber. Adv Ceram Prog. 2018;4:18-23. https://doi.org/ 30501/acp.2018.90829
  14. Shimada S. A thermoanalytical study of oxidation of TiC by simultaneous TGA-DTA-MS analysis. J Mater Sci. 1996;31:673-677. https://doi.org/10.1007/ BF00367884
  15. Zhang C, Boesl B, Agarwal A. Thermal Analysis of Tantalum Carbide-Hafnium Carbide Solid Solutions from Room Temperature to 1400 °C. 2017; 7(8):111. https://doi.org/10.3390/coatings7080111
  16. Hanifi A, Balak Z. Effect of Microstructure, Chemical Composition, and Open Porosity on Oxidation Resistance of ZrB2-Based Composites. Adv Ceram Prog. 2020;6(4): 37-44. https://doi.org/10.30501/acp.2020.204582.1043
  17. Shaker Hashem Al-Habib D, Balak Z, Shahedi Asl M. Spark plasma sinterability of TaC-based composites co-doped with SiC, TiC and graphene. Diam Relat Mater. 2022;130 :109496. https://doi.org/10.1016/j.diamond.2022.109496

 

 

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