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首页> 外文期刊>Journal of engineering materials and technology >Mechanical Behavior of High Temperature Hybrid Carbon Fiber/Titanium Laminates
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Mechanical Behavior of High Temperature Hybrid Carbon Fiber/Titanium Laminates

机译:高温混合碳纤维/钛层压板的力学行为

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摘要

The aim of this paper was to investigate the tensile and flexural properties of hybrid laminates made with titanium sheets and high modulus carbon fiber composites. Grade II titanium was used, which exhibits great high-temperature performance and creep resistance, low weight, and high strength. An inorganic fireproof matrix, known as geopoly-mer, was used to fabricate the high modulus carbon fiber composites. Previous studies have shown that these composites are strong, durable, lightweight, and can exhibit excellent performance up to 400℃. In the present study, a number of specimens were tested in uniaxial tension and four-point bending after exposure at elevated temperatures. The results indicate that the addition of carbon fibers can reduce the weight and increase the stiffness of the pure titanium. Moreover, the hybrid laminates are stronger and stiffer than the sum of the individual strengths and stiffnesses of the parent materials. An important finding is that the interlaminar bond is strong, and as a result no delamination failures were observed.
机译:本文的目的是研究由钛板和高模量碳纤维复合材料制成的混杂层压材料的拉伸和弯曲性能。使用了II级钛,该钛具有出色的高温性能和抗蠕变性,重量轻且强度高。使用无机防火基质(称为地质聚合物)来制造高模量碳纤维复合材料。以前的研究表明,这些复合材料坚固,耐用,轻便,在高达400℃的温度下仍具有出色的性能。在本研究中,在高温下暴露后,对许多样品进行了单轴拉伸和四点弯曲测试。结果表明,碳纤维的添加可以减少纯钛的重量并增加其刚度。而且,混合层压材料比母体材料的单独强度和刚度之和更强和更硬。一个重要的发现是层间键很强,因此没有观察到分层失败。

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