Design and preparation of multilayer TaC/HfC coating: Ablation behavior under oxyacetylene flame with different heat flux

被引:31
作者
Zhang, Jian [1 ]
Zhang, Yulei [1 ]
Zhu, Xiaofei [1 ]
Fu, Yanqin [1 ]
Chen, Ruicong [1 ]
Gai, Wenhan [1 ]
机构
[1] Northwestern Polytech Univ, State Key Lab Solidificat Proc, Shaanxi Key Lab Fiber Reinforced Light Composite M, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
C; C composites; Multilayer; HfC and TaC coating; Ablation resistances; Different heat flux; CARBON-CARBON COMPOSITE; HAFNIUM CARBIDE; CARBON/CARBON COMPOSITE; ANTIOXIDATION PROPERTY; TEMPERATURE-RANGE; CERAMIC COATINGS; OXIDATION; MICROSTRUCTURE; RESISTANCE; DEPOSITION;
D O I
10.1016/j.corsci.2022.110385
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The design of a new multilayer anti-ablation coating is inseparable from the performance assessment in multiple environments. This work investigates the effects of different ablation flux on the microstructure evolution and phase composition of multilayer TaC/HfC coating. The results show that the different temperature regions were generated on ablated coating surface, resulting in the formation of different oxidation products. At heat flux of 2.4 MW/m(2), the formation of dense Hf-Ta-O solid solution phase tightly adhered on substrate. As heat flux increased to 4.2 MW/m(2), a large amount of molten oxidation phase was produced in the central area, which caused secondary damage to the coating under the action of high-speed flame.
引用
收藏
页数:10
相关论文
共 42 条
[1]   CHEMICAL-VAPOR-DEPOSITION OF HAFNIUM CARBIDE AND CHARACTERIZATION OF THE DEPOSITED LAYERS BY SECONDARY-NEUTRAL MASS-SPECTROMETRY [J].
ACHE, HF ;
GOSCHNICK, J ;
SOMMER, M ;
EMIG, G ;
SCHOCH, G ;
WORMER, O .
THIN SOLID FILMS, 1994, 241 (1-2) :356-360
[2]   OXIDATION OF HAFNIUM CARBIDE IN THE TEMPERATURE-RANGE 1400-DEGREES TO 2060-DEGREES-C [J].
BARGERON, CB ;
BENSON, RC ;
JETTE, AN ;
PHILLIPS, TE .
JOURNAL OF THE AMERICAN CERAMIC SOCIETY, 1993, 76 (04) :1040-1046
[3]   Effect of chemical vapor infiltration on erosion and thermal properties of porous carbon/carbon composite thermal insulation [J].
Baxter, RI ;
Rawlings, RD ;
Iwashita, N ;
Sawada, Y .
CARBON, 2000, 38 (03) :441-449
[4]   Texture structure and ablation behavior of TaC coating on carbon/carbon composites [J].
Chen Zhao-Ke ;
Xiong Xiang ;
Li Guo-Dong ;
Sun Wei ;
Long Ying .
APPLIED SURFACE SCIENCE, 2010, 257 (02) :656-661
[5]   Ablation Experiments of Ultra-High-Temperature Ceramic Coating on Carbon-Carbon Composite Using ICP Plasma Wind Tunnel [J].
Chinnaraj, Rajesh Kumar ;
Hong, Seong Min ;
Kim, Ho Seok ;
Oh, Phil Yong ;
Choi, Seong Man .
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 21 (04) :889-905
[6]   Ultra-high-temperature ceramic coatings for oxidation protection of carbon-carbon composites [J].
Corral, Erica L. ;
Loehman, Ronald E. .
JOURNAL OF THE AMERICAN CERAMIC SOCIETY, 2008, 91 (05) :1495-1502
[7]   OXIDATION AND FRACTURE OF A WOVEN 2D CARBON-CARBON COMPOSITE [J].
CROCKER, P ;
MCENANEY, B .
CARBON, 1991, 29 (07) :881-885
[8]   Effect of tantalum carbide on the ablation behaviors of hafnium carbide coating for C/C composites under single and cyclic oxyacetylene torch environments [J].
Feng, Guanghui ;
Li, Hejun ;
Yao, Xiyuan ;
Hu, Dou ;
Yang, Li ;
Li, Bo ;
Lu, Jinhua .
SURFACE & COATINGS TECHNOLOGY, 2020, 400 (400)
[9]   Microstructure and anti-oxidation property of CrSi2-SiC coating for carbon/carbon composites [J].
Fu, QG ;
Li, HJ ;
Shi, XH ;
Liao, XL ;
Li, KZ ;
Huang, M .
APPLIED SURFACE SCIENCE, 2006, 252 (10) :3475-3480
[10]   OXIDATION AND ABLATION OF 3D CARBON-CARBON COMPOSITE AT UP TO 3000-DEGREES-C [J].
HAN, JC ;
HE, XD ;
DU, SY .
CARBON, 1995, 33 (04) :473-478