材料科学
复合材料
极限抗拉强度
航空航天
硅烷
造型(装饰)
模数
政治学
法学
作者
Rubén Seoane-Rivero,Lorena Germán,Fernando Santos,Koldo Gondra
出处
期刊:Polymers
[Multidisciplinary Digital Publishing Institute]
日期:2023-11-10
卷期号:15 (22): 4380-4380
被引量:3
标识
DOI:10.3390/polym15224380
摘要
Nowadays, in the automation and aircraft industries, there is a challenge in minimizing the weight of components of vehicles without losing the original properties. In this study, we fabricate hybrid composites based on fiber metal laminates; these materials could be promising composites for high-performance applications. This work is focused on analyzing the effect of high temperature (175 °C) on the mechanical properties of these kind of materials, by introducing NaOH and silane adhesion treatments between metal and prepreg layers and by using vacuum molding processes. Fabricated FML (NaOH treatment) shows a significant improvement in tensile strength in comparison with the ARALL and GLARE reported by ESA. Moreover, developed FMLs at 175 °C kept more than 70% of their tensile strength and modulus and kept 4% of tensile strain at room temperature. The prominent conclusion achieved in this work has been that excellent candidates have been obtained for a wide range of applications, including but not limited to space and aerospace applications.
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