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Real-time visualization of impact damage in monolithic silicon carbide and fibrous silicon carbide ceramic composite

机译:整体可视化碳化硅和纤维状碳化硅陶瓷复合材料冲击破坏的实时可视化

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Impact resistance from foreign debris is a critical requirement for brittle ceramic and ceramic composite materials intended for use in the hot-section of gas turbine engines. A design to mitigate against such impact failures necessitates a detailed understanding of the driving failure mechanisms. The present study introduces a unique time-resolved experimental method which advances the latter effort. Specifically, a pulsed synchrotron X-ray source, in phase contrast imaging (PCI) configuration, is used as a medium, to visually characterize the evolution of damage inside the target materials during impact. As a proof of concept, two types of ceramic materials were tested: monolithic silicon carbide and fibrous silicon carbide composite. Impact was performed using a light-gas gun and 1.5 mm diameter spheres of partially stabilized zirconia (PSZ) and silicon nitride (Si3N4). The retrieved dynamic X-ray image sequences provided clear outlines of the damage features. In the case of the monolithic ceramic, the impact by a PSZ projectile initially produced a cone crack and complete failure resulted by extension of a median crack. By contrast, the fibrous composite deformed readily prior to cone crack formation. Nearly identical damage features were observed in the monolith for the Si3N4 projectile, with the exception of the added vertical tensile crack. For this same projectile, the fibrous ceramic showed very limited surface deformation and enhanced cone cracking and kinking of laminates along the crack path. The latter response is attributed to the change in projectile properties. Some of the target materials were recovered, and post-mortem analysis via scanning electron microscopy (SEM) showed correlation with observed X-ray damage profiles. Moreover, simple Hertzian contact was used to estimate damage for the elastic portion of impact. This approach was found to yield a reasonable match with experimental results for the surface displacement near the contact interface.
机译:对于用于燃气涡轮发动机热区的脆性陶瓷和陶瓷复合材料,来自异物的抗冲击性是至关重要的要求。为了减轻这种冲击故障的设计,需要对驾驶故障机制有详细的了解。本研究介绍了一种独特的时间分辨实验方法,该方法提高了后者的工作量。具体而言,采用相位对比成像(PCI)配置的脉冲同步加速器X射线源作为介质,以可视方式表征撞击过程中目标材料内部损伤的演变。作为概念验证,测试了两种类型的陶瓷材料:整体式碳化硅和纤维状碳化硅复合材料。使用轻气枪和直径为1.5毫米的部分稳定的氧化锆(PSZ)和氮化硅(Si3N4)的球体进行冲击。检索到的动态X射线图像序列提供了损坏特征的清晰轮廓。在整体陶瓷的情况下,PSZ弹丸的冲击最初会产生圆锥形裂纹,而中位裂纹扩展会导致完全破坏。相比之下,纤维复合材料在形成锥形裂纹之前容易变形。除了增加的垂直拉伸裂纹外,在Si3N4射弹的整体件中观察到几乎相同的破坏特征。对于相同的弹丸,纤维陶瓷显示出非常有限的表面变形,并且沿着裂纹路径增强了层压材料的锥裂和扭结。后一种响应归因于射弹特性的变化。回收了一些目标材料,通过扫描电子显微镜(SEM)进行的事后分析显示与观察到的X射线损伤情况相关。此外,使用简单的赫兹接触来估计冲击弹性部分的损坏。发现该方法与接触界面附近的表面位移的实验结果合理匹配。

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