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首页> 外文期刊>Advanced Composite Materials: The Official Journal of the Japan Society of Composite Materials >The influence of thermal shock on inter-laminar shearing strength of woven C/C composites
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The influence of thermal shock on inter-laminar shearing strength of woven C/C composites

机译:热冲击对机织C / C复合材料层间剪切强度的影响

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Although the mechanical properties of carbon fiber reinforced carbon (C/C) composites under high temperature environments have been widely studied to date, the influence of thermal shocks on C/C composites have scarcely been investigated due to the lack of high-speed heating equipment. Our equipment based on a high frequency induction heating method provided a solution to this problem. In the present study, we examined the influence of thermal shacks on the inter-laminar shearing strength (ILSS), which is one of the most important subjects of designing a plain woven C/C composite with a three point bending test. By the change of the span-to-height ratio (l/h), the failure mode shift of the inter-laminar shearing to the bending was observed. By a series of tests, we proposed an appropriate l/h ratio to obtain a reliable inter-laminar shearing strength of C/C composites, which would be higher than that for the conventional CFRPs. The observation of the failure specimens was done by scanning electron microscopy (SEM) and optical microscopy. Not only debondings at 0 degrees/90 degrees interface but also propagation of transverse cracks were observed in the thermal shocked specimens. The 0 degrees/90 degrees interfacial debondings were suggested as the main source of the inter-laminar shearing strength deterioration. [References: 15]
机译:尽管迄今为止已经广泛研究了高温环境下碳纤维增强碳(C / C)复合材料的机械性能,但是由于缺少高速加热设备,因此几乎没有研究热冲击对C / C复合材料的影响。 。我们基于高频感应​​加热方法的设备解决了这一问题。在本研究中,我们研究了热冲击对层间剪切强度(ILSS)的影响,层间剪切强度是设计具有三点弯曲测试的平纹C / C复合材料的最重要课题之一。通过跨度-高度比(l / h)的变化,观察到层间剪切向弯曲的破坏模式转移。通过一系列测试,我们提出了合适的I / h比值,以获得可靠的C / C复合材料层间剪切强度,该强度将高于常规CFRP。通过扫描电子显微镜(SEM)和光学显微镜对破坏样品进行观察。在热冲击试样中,不仅观察到0度/ 90度界面处的脱胶现象,而且还观察到横向裂纹的扩展。层间剪切强度降低的主要来源被认为是0度/ 90度界面剥离。 [参考:15]

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