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Density, microstructure and mechanical property of large-scale C/C composites prepared by thermal gradient CVI

机译:热梯度CVI制备大型C / C复合材料的密度,微观结构和力学性能

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2D-C/C composites with the dimension of Φ80mm×400mm were prepared rapidly by thermal gradient CVI within 104 hours. Their density reached 1.74g/m~3 and the density difference was less than 0.04g/cm~3. The pyrocarbon microstructure changed from RL to RL+SL, and then to SL along radial direction. These changes were attributed mainly to the difference of gas concentration and temperature gradient at every micro-zone during chemical vapor infiltration. After heat-treatment at high temperature, the space among layers of pyrocarbon enlarged and residual thermal stress was freed, which could lead to cracks formed in matrix. The flexural property of composites decreased with increasing heat-treatment temperature and the fracture mode changed from the brittleness to pseudo-plastic. Carbon particulars between pyrocarbon laminas can increase the flexural strength by particular reinforcement.
机译:在104小时内通过热梯度CVI快速制备尺寸的2D-C / C复合材料,在104小时内快速制备。它们的密度达到1.74g / m〜3,密度差异小于0.04g / cm〜3。从R1到RL + SL的吡磺酰碳微观结构从R1变为径向。这些变化主要归因于化学蒸汽渗透期间每种微区的气体浓度和温度梯度差异。在高温下进行热处理后,释放出扩大和残留的热应力层的层间隙,这可能导致基质中形成的裂缝。复合材料的弯曲性能随着热处理温度的增加而降低,裂缝模式从脆性变为伪塑料。 Pyrocarbon Laminas之间的碳细致可以通过特定的增强来增加弯曲强度。

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