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C/C-ZrC composite prepared by chemical vapor infiltration combined with alloyed reactive melt infiltration

机译:化学气相渗透与合金活性熔体渗透相结合制备的C / C-ZrC复合材料

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摘要

A high performance and low cost C/C-ZrC composite was prepared by chemical vapor infiltration combined with zirconium-silicon (Zr: 91.2 at.%; Si: 8.8 at.%) alloyed reactive melt infiltration. The density of the as-received composite is 2.46 g/cm~3 and the open porosity is 5%. Due to the reaction between the pyrolytic carbon and Zr-Si alloy in the composite, ZrC and Zr_2Si phases were formed, the formation and distribution of which were investigated by thermodynamics and phase diagram. The as-received C/C-ZrC composite, with the flexural strength of 239.5 MPa, displayed a pseudo-ductile fracture behavior. Ablation properties of the C/C-ZrC composite were tested by a pulse laser. The linear ablation rate was 0.028 mm/s. A ZrO_2 barrier layer was formed on the ablation surface and the composite presented excellent ablation resistance.
机译:通过化学气相渗透与锆硅(Zr:91.2 at。%; Si:8.8 at。%)合金化反应熔体渗透相结合,制备了一种高性能,低成本的C / C-ZrC复合材料。接收到的复合材料的密度为2.46 g / cm〜3,开孔率为5%。由于复合材料中热解碳与Zr-Si合金之间的反应,形成了ZrC和Zr_2Si相,并通过热力学和相图研究了它们的形成和分布。弯曲强度为239.5 MPa的C / C-ZrC复合材料表现出拟延性断裂行为。通过脉冲激光测试C / C-ZrC复合材料的烧蚀性能。线性消融速率为0.028mm / s。在烧蚀表面上形成ZrO 2阻挡层,并且该复合材料表现出优异的耐烧蚀性。

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