Ablation Resistant Properties and Mechanism of ZrC Coating Deposited by Plasma-Spraying

被引:0
|
作者
Wen Bo [1 ]
Ma Zhuang [1 ]
Liu Yanbo [1 ]
Wang Fuchi [1 ]
Cai Hongnian [1 ]
机构
[1] Beijing Inst Technol, Lab Sci & Technol Mat Shock & Impact, Beijing 100081, Peoples R China
关键词
C/SiC composite; ablation resistance; plasma spray; ZrC; MICROSTRUCTURE; COMPOSITE; CARBIDE;
D O I
暂无
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The comparatively dense W bonding layer and ZrC ablation-resistant layer were deposited by plasma spraying on C/SiC composite substrate. The ablation resistant properties were tested by oxyacetylene flame. The results show that the coatings have good ablation resistant properties. Ablated by oxyacetylene for 30 mm and 300 s, the mass ablation rate of ZrC coating is 1.7x10(-3) g.s(-1), only 68% of uncoated specimens; linear ablation rate is 4.0x10(-4) mm.s(-1), only 30% of uncoated specimens. With decreasing the ablation distance, the coating mass ablation rate increases, and the linear ablation rate decreases. Because of the temperature gradient caused by the oxyacetylene on the surface of the sample, the coating forms three kinds of ablation apparent morphology after ablation, including the central dense area, the transition area and the edge of loose area. In the central region, WO3 is melted due to high temperature, and effectively fills in the holes and cracks of the coating. In the end, a dense layer is formed, whereupon reducing the mechanical denudation, and the thermochemical corrosion plays a major role. In the marginal area, the ablation products are not melted due to low temperature and they are loose. The anti-ablation forms are mainly thermochemical corrosion and mechanical erosion.
引用
收藏
页码:2782 / 2787
页数:6
相关论文
共 18 条
  • [1] Choury J., 1976, CARBON CARBON MAT NO
  • [2] Effect of heating mode and sintering temperature on the consolidation of 90W-7Ni-3Fe alloys
    Mondal, Avijit
    Upadhyaya, Anish
    Agrawal, Dinesh
    [J]. JOURNAL OF ALLOYS AND COMPOUNDS, 2011, 509 (02) : 301 - 310
  • [3] Materials science - Thermal barrier coatings for gas-turbine engine applications
    Padture, NP
    Gell, M
    Jordan, EH
    [J]. SCIENCE, 2002, 296 (5566) : 280 - 284
  • [4] Pierson HO, 1996, HDB REFRACTORY CARBI, P68
  • [5] The comparison of W/Cu and W/ZrC composites fabricated through hot-press
    Roosta, Mostafa
    Baharvandi, Hamidreza
    [J]. INTERNATIONAL JOURNAL OF REFRACTORY METALS & HARD MATERIALS, 2010, 28 (05): : 587 - 592
  • [6] Advanced ceramic matrix composite materials for current and future propulsion technology applications
    Schmidt, S
    Beyer, S
    Knabe, H
    Immich, H
    Meistring, R
    Gessler, A
    [J]. ACTA ASTRONAUTICA, 2004, 55 (3-9) : 409 - 420
  • [7] Microstructure and ablation properties of zirconium carbide doped carbon/carbon composites
    Shen Xuetao
    Li Kezhi
    Li Hejun
    Du Hongying
    Cao Weifeng
    Lan Fengtao
    [J]. CARBON, 2010, 48 (02) : 344 - 351
  • [8] Song GM, 2001, RARE METAL MAT ENG, V30, P101
  • [9] ZrC ablation protective coating for carbon/carbon composites
    Sun Wei
    Xiong Xiang
    Huang Bai-yun
    Li Guo-dong
    Zhang Hong-bo
    Chen Zhao-ke
    Zheng Xiang-Lin
    [J]. CARBON, 2009, 47 (14) : 3368 - 3371
  • [10] Resistance to ablation of pitch-derived ZrC/C composites
    Tong, QF
    Shi, JL
    Song, YZ
    Guo, QG
    Liu, L
    [J]. CARBON, 2004, 42 (12-13) : 2495 - 2500