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2026, 01, v.45 18-23+29
C/C复合材料表面HfC基涂层的研究进展
基金项目(Foundation): 云南贵金属实验室科技计划项目(YPML-2023050225); 创新团队项目(202405AS350024)
邮箱(Email):
DOI: 10.14078/j.cnki.1001-3741.2026.01.003
摘要:

HfC具有抗氧化、耐烧蚀、导热系数低和固态无相变等优异的性能,是C/C复合材料理想的高温涂层材料之一。但HfC涂层与C/C复合材料之间存在一定的热膨胀系数失配,在热循环冲击下可能从基体上脱落。在HfC涂层与C/C基体之间加入热膨胀系数适中的过渡层(如SiC、TiC等)形成HfC基涂层,过渡层可缓解涂层与基体之间的热应力,高温反应生成的氧化物可有效抑制氧的渗透,提高材料的耐烧蚀性能,延长材料的使用寿命。本文综述了HfC基涂层的制备、组织结构及抗烧蚀性能,并对HfC-PyC梯度涂层进行了热应力模拟,结果表明,在C/C基体与HfC涂层之间增加成分逐步变化的梯度过渡层,可以有效减小基体与涂层之间的残余应力。

Abstract:

HfC has excellent properties such as antioxidant, ablation resistance, low thermal conductivity, and no phase transformation in solid state, making it one of the ideal high-temperature coating materials for C/C composites.However, there is a certain thermal expansion coefficient mismatch between the HfC coating and the C/C substrate, which may cause the coating to fall off from the subs-trate under thermal cycling shock.By introducing a transition layer(such as SiC,TiC,etc.) with a moderate thermal expansion coefficient between the HfC coating and the C/C substrate, a HfC-based coating can be formed.The transition layer can alleviate the thermal stress between the coating and the substrate.Oxides generated at high temperatures can effectively inhibit oxygen permeation, improve the ablation resistance of the material, and extend the service life.This paper reviews the preparation, microstructure, and ablation resistance of HfC-based coatings and presents a thermal stress coupling simulation of HfC-PyC gradient coatings.The results show that adding a gradient transition layer with gradually changing composition between the C/C substrate and HfC coating can effectively reduce the residual stress between the substrate and coating.

参考文献

[1]王富强,陈建,崔红,等.C/C复合材料在核能系统中的应用进展[J].核科学与工程,2020,40(6):1092-1103.

[2]马洪霞,魏晓绛.C/C复合材料在火箭发动机上的应用[J].飞航导弹,2009(3):61-63.

[3]程皓,薛宁娟,侯卫权,等.C/C复合材料在制动系统的应用及发展[J].炭素,2020(3):30-33+29.

[4] Jin X, Fan X, Lu C, et al. Advances in oxidation andablation resistance of high and ultra-high temperature cer-amics modified or coated carbon/carbon composites[J].Journal of the European ceramic Society,2018,38(1):1-28.

[5]王雅雷.C/C复合材料Hf C抗烧蚀涂层的制备、结构及性能研究[D].长沙:中南大学,2012.

[6] Hou X, Chou K C. A simple model for the oxidation ofcarbon-containing composites[J].Corrosion Science,2010,52(3):1093-1097.

[7]宋永忠,翟更太,宋进仁,等.BN改性碳基复合材料氧化行为的研究[J].宇航材料工艺,2001(6):31-33+39.

[8]魏连锋,李克智,吴恒,等.Si C改性C/C复合材料的制备及其烧蚀性能[J].硅酸盐学报,2011,39(2):251-255.

[9] Sun W,Xiong X,Huang B,et al. Zr C ablation protectivecoating for carbon/carbon composites[J].Carbon,2009,47(14):3368-3371.

[10]沈学涛,李克智,李贺军,等.烧蚀产物Zr O2对Zr C改性C/C复合材料烧蚀的影响[J].无机材料学报,2009(5):943-947.

[11]李斌.Ta C陶瓷改性C/C复合材料的设计,制备及其性能[D].长沙:中南大学,2013.

[12]熊翔,王雅雷,李国栋,等.CVI-Si C/Ta C改性C/C复合材料的力学性能及其断裂行为[J].复合材料学报,2008,25(5):91-97.

[13]李淑萍,李克智,郭领军,等.Hf C改性C/C复合材料整体喉衬的烧蚀性能研究[J].无机材料学报,2008,23(6):1155-1158.

[14] Sun H H, Li H J, Shen X T, et al. Microstructure andablation behavior of C/C composites doped with Zr B2[J]. Journal of Inorganic Materials,2011,26(6):669-672.

[15]宋永忠,翟更太,宋进仁,等.BN改性碳基复合材料氧化行为的研究[J].宇航材料工艺,2001,31(6):31-39.

[16] Corral E L,Walker L S. Improved ablation resistance ofC/C composites using zirconium diboride and boroncarbide[J]. Journal of the European Ceramic Society,2010,30(11):2357-2364.

[17] Wang Y J,Li H J,Fu Q G,et al. Ablative property ofHf C-based multilayer coating for C/C compo-sites underoxy-acetylene torch[J]. Applied Surface Science,2011,257(10):4760-4763.

[18] Zhong L,Guo L J,Huang J,et al.Ablation behavior of theZr C coating on C/C composite with the construction ofthermal dispersal network[J]. Ceramics International,2023,49(9):13903-13915.

[19] Chen Z, Wu W, Cheng H, et al. Microstructure andevolution of iridium coating on the C/C composites abl-ated by oxyacetylene torch[J].Acta Astronautica,2010,66(5-6):682-687.

[20] Sayir A.Carbon fiber reinforced hafnium carbide compo-site[J].Journal of Materials Science,2004,39(19):5995-6003.

[21] Wang Y L,Xiong X,Li G D,et al. Ablation behavior ofHf C protective coatings for carbon/carbon composites inan oxyacetylene combustion flame[J].Corrosion Science,2012,65:549-555.

[22] Li G Q,Li G Y.Microstructure and mechanical propertiesof hafnium carbide coatings synthesized by reactive mag-netron sputtering[J].Journal of Coatings Technology andResearch,2010,7(3):403-407.

[23]侯根良,苏勋家,王延斌,等.C/C复合材料抗烧蚀Hf C涂层的制备[J].航空材料学报,2009,29(1):77-80.

[24] Zhang J,Zhang Y,Fu Y,et al.Ablation behavior of Hf Ccoating with different thickness for carbon/carbon comp-osites at ultra-high temperature[J]. Journal of the Euro-pean Ceramic Society,2021,41(3):1769-1778.

[25]郑鹏,李红,杨敏,等.C/C-Hf C复合材料的抗烧蚀性能[J].材料工程,2024,52(5):171-178.

[26] Fu Y,Zhang Y,Zhang J,et al.Mechanical properties andablation resistance of Hf C nanowire modified carbon/car-bon composites[J]. Ceramics International, 2020, 46(10):16142-16150.

[27] Talwar D N,Sherbondy J C.Thermal expansion coefficientof 3C-Si C[J]. Applied Physics Letters,1995,67(22):3301-3303.

[28]黄会晗,李同起,徐林,等.C/C复合材料抗氧化涂层制备工艺研究进展[J].炭素技术,2024,43(4):1-10.

[29] Ren J,Zhang Y,Fu Y,et al.Effects of the second phaseon the microstructure and ablation resistance of Hf Ccoating on C/C composites[J].Surface&Coatings Tec-hnology,2018,344:250-258.

[30] Kim H S,Kang B R,Choi S M. Fabrication and chara-cteristics of a Hf C/Ti C multilayer coating by a vacuumplasma spray process to protect C/C composites againstoxidation[J].Corrosion Science,2021,178:109068.

[31] Feng G,Li H,Yao X,et al. Ablation resistance of Hf C-Ta C/Hf C-Si C alternate coating for Si C-coated carbon/carbon composites under cyclic ablation[J].Journal of theEuropean Ceramic Society,2021,41(6):3207-3218.

[32]张瑞涛,杨鑫,王秀飞,等.Hf C-Si C复合涂层的制备及高温耐烧蚀性能研究[J].炭素技术,2021,40(6):38-42+55.

[33] Zhang J, Zhang Y, Fu Y, et al. Growth mechanism andablation behavior of CVD-Hf C coating on the surface ofC/C composites and CVD-Si C coating[J].Corrosion Sci-ence,2021,192:109819

[34]杨旸.Hf C复合涂层的SAPS制备和抗烧蚀性能研究[D].西安:西北工业大学,2017.

[35] Ren J,Zhang Y,Zhang P,et al.Ablation resistance of Hf C coating reinforced by Hf C nanowires in cyclic ablationenvironment[J]. Journal of the European Ceramic Soc-iety,2017,37(8):2759-2768.

[36] Li K Z,Duan T,Zhang J P,et al.Ablation mechanism ofcarbon/carbon composites modified by Hf C-Si C in twoconditions under oxyacetylene torch[J]. Journal of Mat-erials Science&Technology,2017,33(1):71-78.

[37] Hou W,Feng T,Meng X,et al. Ablation behaviors andmechanisms of Cf/Hf CPIP-Si CCVIcomposites:From Si O2nanowires film to Hf O2skeleton[J]. Corrosion Science,2022,209:110766.

[38] Zhang J,Xin Y,Wang R,et al.Ablation behaviour of C/C-Hf C-Si C composites prepared by joint route of precu-rsor infiltration and pyrolysis and gaseous silicon infiltr-ation[J].Chinese Journal of Aeronautics,2023,36(9):426-436.

[39] Duan L,Zhao X,Wang Y.Comparative ablation behaviorsof C/Si C-Hf C composites prepared by reactive melt infil-tration and precursor infiltration and pyrolysis routes[J].Ceramics International,2017,43(18):16114.

[40] Yan C,Liu R,Zha B,et al.Fabrication and properties of3-dimensional 4-directional Cf/Hf C-Si C composites byprecursor impregnation and pyrolysis process[J].Journalof Alloys and Compounds,2018,739:955-960.

[41] Lu J,Hao K,Liu L,et al.Ablation resistance of Si C-Hf C-Zr C multiphase modified carbon/carbon composites[J].Corrosion Science,2016,103:1-9.

基本信息:

DOI:10.14078/j.cnki.1001-3741.2026.01.003

中图分类号:TB332;TB306

引用信息:

[1]王献,汪星强,魏燕,等.C/C复合材料表面HfC基涂层的研究进展[J].炭素技术,2026,45(01):18-23+29.DOI:10.14078/j.cnki.1001-3741.2026.01.003.

基金信息:

云南贵金属实验室科技计划项目(YPML-2023050225); 创新团队项目(202405AS350024)

投稿时间:

2025-01-08

投稿日期(年):

2025

终审时间:

2025-01-20

终审日期(年):

2025

审稿周期(年):

1

发布时间:

2026-02-25

出版时间:

2026-02-25

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