欢迎登录材料期刊网

材料期刊网

高级检索

本研究在炭/炭复合材料热解炭基体织构形成与转化的模型基础上,基于石墨微晶片层的表面结构特点,建立了蜂窝结构的热解炭沉积表面几何模型,并运用Monte Carlo方法模拟了在等温等压化学气相渗透(CVI)过程中热解炭基体沉积的动力学过程,研究了预制体比表面积(As/VR)和入口气体分压对热解炭微观结构的影响.通过数值模拟并结合已公开发表的实验结果发现,在CVI工艺过程中一定的压力条件下,通过控制As/VR可以获得不同织构的热解炭,预制体的As/VR存在两个临界值,靠近反应器入口处的临界值为1.45 m-1和8.9 mm-1,靠近反应器出口处的临界值为0.3mm-1,当As/VR处于这两个临界值之间时,系统主要沉积高织构热解炭;在同一As/VR且压强小于30 kPa的条件下,通过控制反应气体压强的值也可以得到不同织构的热解炭,并且压强也存在一个临界值,当压强大于这个临界值时,系统主要沉积高织构热解炭.

参考文献

[1] Luo RY;Liu T;Li JS;Zhang HB;Chen ZJ;Tian GL.Thermophysical properties of carbon/carbon composites and physical mechanism of thermal expansion and thermal conductivity[J].Carbon: An International Journal Sponsored by the American Carbon Society,200414(14):2887-2895.
[2] S. CHAND.Review Carbon fibers for composites[J].Journal of Materials Science,20006(6):1303-1313.
[3] Guellali M;Oberacker R;Hoffmann MJ.Influence of the matrix microstructure on the mechanical properties of CVI-infiltrated carbon fiber felts[J].Carbon: An International Journal Sponsored by the American Carbon Society,20059(9):1954-1960.
[4] 张丹;黄清波;李爱军;白瑞成;孙晋良.碳/碳复合材料热解碳基体的织构界面形成机制Monte Carlo模拟[J].复合材料学报,2014(4):859-865.
[5] B.Reznik;D.Gerthsen.Microscopic study of failure mechanisms in infiltrated carbon fiber felts[J].Carbon: An International Journal Sponsored by the American Carbon Society,20031(1):57-69.
[6] Z.J.Hu;W.G.Zhang;K.J.Huttinger;B.Reznik;D.Gerthsen.Influence of pressure, temperature and surface area/volume ratio on the texture of pyrolytic carbon deposited from methane[J].Carbon: An International Journal Sponsored by the American Carbon Society,20034(4):749-758.
[7] B. Reznik;K.J. Huttinger.On the terminology for Pyrolytic carbon[J].Carbon: An International Journal Sponsored by the American Carbon Society,20024(4):621-624.
[8] Dong GL.;Huttinger KJ..Consideration of reaction mechanisms leading to pyrolytic carbon of different textures[J].Carbon: An International Journal Sponsored by the American Carbon Society,200214(14):2515-2528.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%