首页> 外文期刊>Vacuum: Technology Applications & Ion Physics: The International Journal & Abstracting Service for Vacuum Science & Technology >Thermal ablation behavior of SiC coating for 3D braided carbon fiber reinforced ZrC-SiC composites in different heat fluxes
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Thermal ablation behavior of SiC coating for 3D braided carbon fiber reinforced ZrC-SiC composites in different heat fluxes

机译:三维编织碳纤维增强Zrc-SiC复合材料在不同热量通量的热消融行为

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摘要

In this study, CVD-SiC coating was prepared on 3D braided carbon fiber reinforced ZrC-SiC (abbreviated as C-f/ZrC-SiC) composites, and the microstructure and morphology of the composites and coating were characterized by scanning electron microscopy coupled with energy dispersive spectrometry (SEM-EDS), X-ray diffraction (XRD). The effect and mechanism of CVD-SiC coating on the ablation properties of C-f/ZrC-SiC composites under different ablation conditions were studied in details. The results showed that the CVD-SiC coating could reduce the ablation temperature and improve the compactness, which will promote the ablation properties of the C-f/ZrC-SiC composites in the heat flux of 2.38 MW/m(2). But with the heat flux increasing to 4.18 MW/m(2), ablation properties of C-f/ZrC-SiC composites decreased significantly, it was mainly difficult to form dense and stable ZrO2-SiO2 protective oxides due to accelerated mechanical erosion which makes the CVD-SiC coating lose its protection for C-f/ZrC-SiC composites during ablation and higher ablation temperature which will aggravate active oxidation of SiC and the evaporation of SiO2.
机译:在该研究中,在3D编织碳纤维增强ZrC-SiC(缩写为CF / ZrC-SiC)复合材料上制备CVD-SiC涂层,并通过扫描电子显微镜与能量分散扫描的电子显微镜表征复合材料和涂层的微观结构和形态光谱法(SEM-EDS),X射线衍射(XRD)。研究了CVD-SIC涂层对不同消融条件下C-F / ZrC-SiC复合材料的消融性质的影响和机理。结果表明,CVD-SiC涂层可以降低消融温度并改善紧凑性,促进C-F / Zrc-SiC复合材料的热通量在2.38mW / m(2)中的烧蚀性能。但随着加热通量增加到4.18mW / m(2),Cf / Zrc-SiC复合材料的消融性能显着降低,主要是由于加速机械侵蚀而形成致密且稳定的ZrO2-SiO2保护氧化物,这使得CVD -SIC涂层在消融和更高的消融温度期间对CF / ZrC-SiC复合材料的保护失去了对SiC的活性氧化和SiO 2的蒸发的粘合温度。

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