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首页> 外文期刊>Surface & Coatings Technology >Ablation mechanism mechanism of ZrB2-SiC coating for SiC-coated graphite under an oxyacetylene flame
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Ablation mechanism mechanism of ZrB2-SiC coating for SiC-coated graphite under an oxyacetylene flame

机译:氧乙炔火焰下SiC涂层石墨锌2-SiC涂层的烧蚀机理

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摘要

ZrB2-SiC coating was fabricated on SiC-coated graphite using shrouded plasma spray (SPS). Ablation resistance of the coating was evaluated through oxyacetylene for 15 s, 30 s, 120 s and 360 s. The sample weight has increased after ablation for 15 s, 30 s and 120 s with generation of oxide products. The ZrO2 layer was produced from ZrB2-SiC oxidation and acted as a thermal barrier. In the case of 360 s ablation, the SiC inner layer is oxidized and evaporated and a gap remained between ZrO2 layer and graphite. Phase transformation of ZrO2 during cooling induces the volume expansion. As a result, cracks are generated in the central region during cooling from high temperature to room temperature.
机译:使用罩等离子喷雾(SPS)在SiC涂层石墨上制造ZrB2-SiC涂层。 通过羟乙烯评价涂层的消融抗性15s,30s,120s和360s。 在消融15s,30s和120秒后,样品重量增加了氧化物产物。 ZrO2层由ZrB2-SiC氧化制备,并用作热屏障。 在360秒消融的情况下,SiC内层被氧化并蒸发,并且在Zro2层和石墨之间保持间隙。 冷却过程中ZrO2的相变诱导体积膨胀。 结果,在从高温下冷却至室温期间在中心区域中产生裂缝。

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