Effect of CVD-SiC array structure on ablation resistance of ZrB2/SiC coatings

被引:0
|
作者
Gao Z. [1 ,2 ]
Ma Z. [1 ,2 ]
Liu Y. [1 ,2 ]
机构
[1] School of Materials Science and Engineering, Beijing Institute of Technology, Beijing
[2] Chongqing Innovation Center, Beijing Institute of Technology, Chongqing
关键词
ablation; array structure; C/C composite materials; CVD-SiC; laser etching; plasma spraying;
D O I
10.7527/S1000-6893.2023.28842
中图分类号
学科分类号
摘要
Influence of array structure on the performance of ZrB2/SiC coatings was studied by using femtosecond laser to prepare arrays with different sizes on the surface of the Chemical Vapor Deposition(CVD)-SiC interlayer. Results showed that with the increase of laser etching frequency,the depth of the array structure increased from 30 μm to 150 μm. After 600 s of oxyacetylene combustion,the surface temperature of the ZrB2/SiC coating decreased gradually with the increase of CVD-SiC microstructure depth,and the lowest surface temperature reached 1 700 ℃,which decreased by nearly 200 ℃ . The color of the combustion center area transitioned from white to light gray. For the samples with an etching frequency of 5 times,after a single cycle of 600 s,the mass combustion rate and linear combustion rate were -7. 4 × 10-5 g/s and -13. 3 μm/s respectively. The array structure increased the contact area between the ZrB2/SiC coating and the CVD-SiC interlayer,thereby increasing the thermal conductivity,reducing heat accumulation,and ultimately enhancing the anti-combustion performance of the ZrB2/SiC coating. © 2024 Chinese Society of Astronautics. All rights reserved.
引用
收藏
相关论文
共 26 条
  • [1] KIM J H,, Et al., Evaluation of oxidation behaviors of HfC-SiC ultra-high temperature ceramics at above 2500℃ via oxyacetylene torch[J], Ceramics International, 44, 7, pp. 8505-8513, (2018)
  • [2] YANG S J, YAN X D, GUO H B., Failure mechanism and protection strategy of thermal barrier coatings under CMAS attack[J], Acta Aeronautica et Astronautica Sinica, 43, 10, (2022)
  • [3] ZHENG H, YUAN S F,, Et al., Experimental method of guided wave monitoring for high temperature airflow damage of C/C thermal protection structures[J], Acta Aeronautica et Astronautica Sinica, 43, 8, (2022)
  • [4] LI H, ZOU Z Y,, Et al., Analysis and verification of nonlinear vibrations of fiber-reinforced composite cylindrical shells in thermal environment[J], Acta Aeronautica et Astronautica Sinica, 43, 9, (2022)
  • [5] LI D J, YANG L Y,, SUN F,, Et al., Effect of preheating temperature on formation of surface cracks in thermal barrier coating system[J], Acta Aeronautica et Astronautica Sinica, 43, 6, (2022)
  • [6] VAN WIE D M,, DREWRY D G,, KING D E,, Et al., The hypersonic environment:Required operating conditions and design challenges[J], Journal of Materials Science, 39, 19, pp. 5915-5924, (2004)
  • [7] YANG Z X, NI L Y,, YANG J, Et al., Microstructure and radiation property of Tb<sub>4</sub>O<sub>7</sub> doped Cr<sub>2</sub>O<sub>3</sub>-TiO<sub>2</sub>based high emissivity coating[J], Surface Technology, 47, 5, pp. 154-158, (2018)
  • [8] WU Q R, WEN B X., Studies on the thermo-physical properties of SiC heat exchanger materials[J], Journal of Inorganic Materials, 11, 2, pp. 333-337, (1996)
  • [9] PARK J E, Et al., State of the art of high heat flux cooling technologies[J], Heat Transfer Engineering, 28, 4, pp. 258-281, (2007)
  • [10] JIANG D F,, LONG J Y, CAI M Y,, Et al., Femtosecond laser fabricated micro/nano interface structures toward enhanced bonding strength and heat transfer capability of W/Cu joining[J], Materials and Design, 114, pp. 185-193, (2017)