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Ablation, Thermal, and Morphological Properties of SiC Fiber-Reinforced Ceramic Matrix Composites

机译:SiC纤维增强陶瓷基复合材料的烧蚀,热和形态学性能

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This research encompassed the characterization of three novel Ceramic Matrix Composites (CMCs) in order to predict their performances in hypersonic applications. Ablation, thermal, and morphological properties of these CMC materials were characterized by in-situ ablation sensors, thermogravimetric analyses, and scanning electron microscopy (SEM) observations, respectively. The in-situ ablation sensor made use of four O.S mm thermocouples which were mounted into the sample at staggered depths after the sample had been micro-drilled. As the surface eroded and the recession front advanced, thermocouples would break, resulting in a unique timestamp as the front passed each one. Plotting the recession penetration as a result of these timestamps and superimposing a trendline yielded the recession rate for each material. Thermal testing proved the PyroSic? composites retain virtually all their mass when exposed to high-temperature environments, never losing more than 1.5% of their mass. The Korean CMC, on the other hand, did not perform as well, retaining only 55% of its original mass when subjected to a 5°C/min rate of temperature elevation. Higher rates of elevation tended to mitigate the loss of material. Morphological characterization aimed to compare the microstructural features before and after ablation testing. As expected, the scorched surface showed many traits indicative of prolonged thermal stress, including hairline fractures, distortions of the glass ceramic matrix, and splintering of fibers. The combination of these attributes promotes a degree of disorder into the composite, diminishing its ability to resist further thermal and mechanical stress. Moreover, at a heat flux of 1000 W/cm~2, the mean recession rates of the PyroSic? 2704 and PyroSic? 4686 samples were 0.0231 and 0.0148 mm/s, respectively, representing a difference of 56%. Although this research provides valuable insight into the properties of these CMCs, future trials will need to be conducted to confirm the results and account for statistical variance.
机译:该研究包括三种新型陶瓷基复合材料(CMC)的表征,以预测其在超音速应用中的性能。通过原位消融传感器,热重分析和扫描电子显微镜(SEM)观察,本谱的消融,热和形态学性质的特征在于分别的原位消融传感器。原位消融传感器采用四个O.S MM热电偶在样品微钻后在交错深度安装到样品中。随着表面侵蚀和经济衰退前进的先进,热电偶会破裂,导致正面通过每一个时的唯一时间戳。由于这些时间戳和叠加趋势线的结果,绘制经济衰退渗透率产生了每种材料的衰退率。热试验证明了蛋白质?复合材料在暴露于高温环境时,几乎所有的质量都在,从未失去超过1.5%的质量。另一方面,韩国CMC也没有表现,在经过5°C /最小的温度升高速率时,仅保留其原始质量的55%。提高升高率倾向于减轻物料的损失。形态学特征旨在比较烧蚀试验前后的微观结构特征。如预期的那样,烧焦的表面显示出许多指示延长热应力的特征,包括吹风性裂缝,玻璃陶瓷基质的扭曲和纤维的碎片。这些属性的组合将一定程度的无序程度促进到复合材料中,减少其抵抗进一步热和机械应力的能力。另外,在1000W / cm〜2的热通量下,蛋白的平均衰退率? 2704和溶解? 4686样品分别为0.0231和0.0148mm / s,表示差异为56%。虽然这项研究提供了对这些CMC的性质的宝贵洞察,但需要进行未来的试验,以确认结果并占统计方差。

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