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Preparing antioxidant coatings to address the inherent oxidation sensitivity of carbon fiber-reinforced carbon aerogel (C/CA) composites is a feasible way to promote their application in oxidizing environments as thermal insulation materials. However, preparing the coatings with excellent oxidation and ablation resistance while avoiding evident damage to the C/CA substrate still remains a challenge. Herein, a SiC@SiO2 nanowire-toughened ZrB2–SiC/SiC bilayer coating with a large thickness of 500 μm was prepared on C/CA using a one-step low-temperature reaction sintering method, which simultaneously formed a sintered outer layer with even-distributed nanowires and a siliconized gradient inner layer. By courtesy of the synergic thermal response of the layers and the crack deflection induced by the nanowires, the resulting coating has moderate residual compressive stress of 0.08–1.22 GPa in the interface, high interfacial bonding strength of 6.02 MPa, and good fracture toughness of 4.36 MPa·m1/2. Benefited from the optimum components and improved structure, the coating shows excellent cyclic ablation resistance with linear ablation rates of 0.1 μm/s at 1650 for 1500 s (300 s × 5 cycles) and 0.4 μm/s at 1850 for 900 s (300 s × 3 cycles). The one-step preparation strategy contributes to little damage to the substrate, thus showing the well-preserved mechanical and thermal insulation properties.


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Facile preparation of a SiC@SiO2 nanowire-toughened ZrB2–SiC/SiC bilayer coating with good interfacial bonding, high toughness, and excellent cyclic ablation resistance on C/CA composites

Show Author's information Meng Yan1,2Chenglong Hu1( )Jian Li1Shengyang Pang1Bohui Sun1Rida Zhao1Bin Liang1Rui Luo1,2Sufang Tang1( )
Shi-Changxu Innovation Center for Advanced Materials, Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China
School of Materials Science and Engineering, University of Science and Technology of China, Shenyang 110016, China

Abstract

Preparing antioxidant coatings to address the inherent oxidation sensitivity of carbon fiber-reinforced carbon aerogel (C/CA) composites is a feasible way to promote their application in oxidizing environments as thermal insulation materials. However, preparing the coatings with excellent oxidation and ablation resistance while avoiding evident damage to the C/CA substrate still remains a challenge. Herein, a SiC@SiO2 nanowire-toughened ZrB2–SiC/SiC bilayer coating with a large thickness of 500 μm was prepared on C/CA using a one-step low-temperature reaction sintering method, which simultaneously formed a sintered outer layer with even-distributed nanowires and a siliconized gradient inner layer. By courtesy of the synergic thermal response of the layers and the crack deflection induced by the nanowires, the resulting coating has moderate residual compressive stress of 0.08–1.22 GPa in the interface, high interfacial bonding strength of 6.02 MPa, and good fracture toughness of 4.36 MPa·m1/2. Benefited from the optimum components and improved structure, the coating shows excellent cyclic ablation resistance with linear ablation rates of 0.1 μm/s at 1650 for 1500 s (300 s × 5 cycles) and 0.4 μm/s at 1850 for 900 s (300 s × 3 cycles). The one-step preparation strategy contributes to little damage to the substrate, thus showing the well-preserved mechanical and thermal insulation properties.

Keywords: coating, interface, residual stress, toughness, carbon fiber reinforced carbon aerogel (C/CA) composites

References(40)

[1]

ElKhatat AM, Al-Muhtaseb SA. Advances in tailoring resorcinol-formaldehyde organic and carbon gels. Adv Mater 2011, 23: 2887–2903.

[2]

Ma J, Li J, Guo PL, et al. Tailoring microstructures of carbon fiber reinforced carbon aerogel-like matrix composites by carbonization to modulate their mechanical properties and thermal conductivities. Carbon 2022, 196: 807–818.

[3]

Guo PL, Li J, Pang SY, et al. Ultralight carbon fiber felt reinforced monolithic carbon aerogel composites with excellent thermal insulation performance. Carbon 2021, 183: 525–529.

[4]

Xiao YY, Liu SH, Zhou JL, et al. Lightweight, strong, and thermally insulating polybenzoxazine aerogel thermal protection composites for antioxidant ablation long to 1800 s. Compos Part B Eng 2023, 266: 111045.

[5]

Zhang WW, Hu CL, Li J, et al. Insight into the origin of oxidation behaviors of carbon fiber reinforced carbon aerogel composites with different porous skeletons. Carbon 2023, 209: 118008.

[6]

Yan M, Hu CL, Li J, et al. Construction of a ceramic coating with low residual stress on C/CA composites for thermal protection at ultra-high temperatures. Compos Part B Eng 2023, 266: 110970.

[7]

Hu D, Fu QG, Zhou L, et al. Effects of air plasma flame on the ZrB2-based UHTC coatings: Microstructure, phase evolution and ablation resistance. J Mater Sci Technol 2023, 158: 194–206.

[8]

Shi HL, Zhang ML, Zhou L, et al. Improved oxidation protective ability of SHS powder-synthesized ZrB2–MoSi2–SiC–Si coating on carbon/carbon composites. Surf Coat Technol 2022, 447: 128838.

[9]

Zhou L, Fu QG, Hu D, et al. A dense ZrB2–SiC–Si/SiC–Si coating to protect carbon/carbon composites against oxidation at 1773 K and 1973 K. Corros Sci 2021, 183: 109331.

[10]

Li T, Zhang YL, Li JC, et al. Improved mechanical strength and oxidation resistance of SiC/SiC–MoSi2–ZrB2 coated C/C composites by a novel strategy. Corros Sci 2022, 205: 110419.

[11]

Li T, Zhang YL, Lv JS, et al. Eliminated siliconization corrosion and improved oxidation resistances of SiC–Si coated C/C composites via a ZrB2-rich transition layer. Corros Sci 2022, 195: 109986.

[12]

Zhu XF, Zhang YL, Zhang J, et al. SiC/HfB2-based ceramic/SiC multilayer coating to protect C/C composites against oxidation at medium and high temperatures for long-life service. Corros Sci 2022, 201: 110299.

[13]

Zhang J, Zhang YL, Zhu XF, et al. Design and preparation of multilayer TaC/HfC coating: Ablation behavior under oxyacetylene flame with different heat flux. Corros Sci 2022, 204: 110385.

[14]

Zhang J, Zhang YL, Fu YQ, et al. Long-time ablation behavior of the multilayer alternating CVD-(SiC/HfC)3 coating for carbon/carbon composites. Corros Sci 2021, 189: 109586.

[15]

Ren JC, Zhang YL, Zhang PF, et al. UHTC coating reinforced by HfC nanowires against ablation for C/C composites. Surf Coat Technol 2017, 311: 191–198.

[16]

Wang KL, Zhu JP, Wang HL, et al. Air plasma-sprayed high-entropy (Y0.2Yb0.2Lu0.2Eu0.2Er0.2)3Al5O12 coating with high thermal protection performance. J Adv Ceram 2022, 11: 1571–1582.

[17]

Wei ZY, Meng GH, Chen L, et al. Progress in ceramic materials and structure design toward advanced thermal barrier coatings. J Adv Ceram 2022, 11: 985–1068.

[18]

Nance J, Subhash G, Sankar B, et al. Measurement of residual stress in silicon carbide fibers of tubular composites using Raman spectroscopy. Acta Mater 2021, 217: 117164.

[19]

Ghosh D, Subhash G, Orlovskaya N. Measurement of scratch-induced residual stress within SiC grains in ZrB2–SiC composite using micro-Raman spectroscopy. Acta Mater 2008, 56: 5345–5354.

[20]

Niu XX, Zhang HQ, Pei ZL, et al. Measurement of interfacial residual stress in SiC fiber reinforced Ni–Cr–Al alloy composites by Raman spectroscopy. J Mater Sci Technol 2019, 35: 88–93.

[21]

Faisal NH, Reuben RL, Ahmed R. An improved measurement of Vickers indentation behaviour through enhanced instrumentation. Meas Sci Technol 2011, 22: 015703.

[22]

Faisal NH, Ahmed R, Prathuru AK, et al. An improved Vickers indentation fracture toughness model to assess the quality of thermally sprayed coatings. Eng Fract Mech 2014, 128: 189–204.

[23]

Yan M, Hu CL, Li J, et al. An unusual carbon–ceramic composite with gradients in composition and porosity delivering outstanding thermal protection performance up to 1900 ℃. Adv Funct Mater 2022, 32: 2204133.

[24]

Fu YQ, Zhang YL, Chen H, et al. Ultra-high temperature performance of carbon fiber composite reinforced by HfC nanowires: A promising lightweight composites for aerospace engineering. Compos Part B Eng 2023, 250: 110453.

[25]
Yan NN, Shi XH, Li K, et al. In-situ homogeneous growth of ZrC nanowires on carbon cloth and their effects on flexural properties of carbon/carbon composites. Compos Part B Eng 2018, 154 : 200–208.
DOI
[26]

Liu DC, Jing YZ, Cui XF, et al. Study of toughening behavior of SiC whiskers on 8YSZ thermal barrier coatings. Surf Coat Technol 2023, 455: 129232.

[27]

Bobzin K, Zhao L, Heinemann H, et al. Effect of heat treatment on the structure, fracture toughness and oxidation behavior of a silicon coating by atmospheric plasma spraying. Surf Coat Technol 2023, 472: 129965.

[28]

Li B, Li HJ, Yao XY, et al. Preparation and ablation resistance of ZrC nanowires-reinforced CVD-ZrC coating on sharp leading edge C/C composites. Appl Surf Sci 2022, 584: 152617.

[29]

Tian XF, Yang L, Li B, Li HJ, Shi XH, Lin HJ. Ablation behaviors of SiC nanowire-reinforced ZrC–SiC coating-matrix integrated C/C composites with different ratios of precursors. J Eur Ceram Soc 2022, 42: 6774–6784.

[30]

Chen PJ, Xiao P, Tang X, et al. Corrosion behavior and failure mechanism of SiC whisker and c-AlPO4 particle-modified novel tri-layer Yb2Si2O7/mullite/SiC coating in burner rig tests. J Adv Ceram 2022, 11: 1901–1917.

[31]

Wang RQ, Wang N, Zhu SZ, et al. Study on the mechanism of ultra-high temperature ablation of ZrB2–SiC–TaSi2 coatings by low-pressure plasma spraying on the C/C composites. Ceram Int 2023, 49: 11344–11354

[32]

Karlsdottir SN, Halloran JW. Oxidation of ZrB2–SiC: Influence of SiC content on solid and liquid oxide phase formation. J Am Ceram Soc 2009, 92: 481–486.

[33]

Qian DY, Chen YX, Ren XR, et al. Effect of La2O3 content on the oxygen barrier ability of the HfB2–SiC coating at 1973 K. J Am Ceram Soc 2023, 106: 2155–2168.

[34]

Zhang ML, Ren XR, Zhang MC, et al. Preparation of ZrB2–MoSi2 high oxygen resistant coating using nonequilibrium state powders by self-propagating high-temperature synthesis. J Adv Ceram 2021, 10: 1011–1024.

[35]

Torabi S, Valefi Z, Ehsani N. Ablation behavior of SiC/ZrB2 ultra-high temperature ceramic coatings by solid shielding shrouded plasma spray for high-temperature applications (temperature above 2000 ℃). Surf Coat Technol 2020, 403: 126271.

[36]

Tan W, Adducci M, Trice R. Evaluation of rare-earth modified ZrB2–SiC ablation resistance using an oxyacetylene torch. J Am Ceram Soc 2014, 97: 2639–2645.

[37]

Sun GD, Li HJ, Yao DJ, et al. A multilayer SiC/ZrB2/SiC ablation resistance coating for carbon/carbon composites. Adv Eng Mater 2019, 21: 1800774.

[38]

Li CY, Li GB, Ouyang HB, et al. ZrB2 particles reinforced glass coating for oxidation protection of carbon/carbon composites. J Adv Ceram 2019, 8: 102–111.

[39]

Xiao CX, Song Q, Shen QL, et al. Understanding on interlaminar nano-reinforcement induced mechanical performance improvement of carbon/carbon composites after silicon infiltration. Compos Part B Eng 2022, 239: 109946.

[40]

Quan HF, Wang LY, Huang JT, et al. Durable protection and failure mechanism of the multilayer coating system for SiCf/SiC composites under high-temperature oxidation. Compos Part B Eng 2022, 244: 110197.

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Received: 16 January 2024
Revised: 21 February 2024
Accepted: 28 February 2024
Published: 30 April 2024
Issue date: April 2024

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© The Author(s) 2024.

Acknowledgements

Acknowledgements

This work has been supported by the Defense Industrial Technology Development Program (No. JCKY2021130B007), the National Natural Science Foundation of China (Nos. 52272075 and 52188101), the Research Fund of Youth Innovation Promotion Association of Chinese Academy of Sciences (No. 2021190), the directional institutionalized scientific research platform relies on China Spallation Neutron Source of Chinese Academy of Sciences, and the National Key R&D Program of China (No. 2021YFA1500804).

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This is an open access article under the terms of the Creative Commons Attribution 4.0 International License (CC BY 4.0, http://creativecommons.org/licenses/by/4.0/).

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