Crashworthiness characteristics of a carbon fiber reinforced dual-phase epoxy–polyurea hybrid matrix composite

التفاصيل البيبلوغرافية
العنوان: Crashworthiness characteristics of a carbon fiber reinforced dual-phase epoxy–polyurea hybrid matrix composite
المؤلفون: Thomas L. Attard, Yanli Wang, Kittinan Dhiradhamvit, Hongyu Zhou, Donald L. Erdman
المصدر: Composites Part B: Engineering. 71:17-27
بيانات النشر: Elsevier BV, 2015.
سنة النشر: 2015
مصطلحات موضوعية: Materials science, Scanning electron microscope, Mechanical Engineering, Composite number, Thermosetting polymer, Epoxy, Elastomer, Industrial and Manufacturing Engineering, chemistry.chemical_compound, chemistry, Mechanics of Materials, visual_art, visual_art.visual_art_medium, Ceramics and Composites, Crashworthiness, Composite material, Damage tolerance, Polyurea
الوصف: The crashworthiness characteristics of rectangular tubes made from a Carbon-fiber reinforced Hybrid-Polymeric Matrix (CHMC) composite were investigated using quasi-static and impact crush tests. The hybrid matrix formulation of the CHMC was created by combining an epoxy-based thermosetting polymer with a lightly crosslinked polyurea elastomer at various cure-time intervals and volumetric ratios. The load–displacement responses of both CHMC and carbon-fiber reinforced epoxy (CF/epoxy) specimens were obtained under various crushing speeds; and crashworthiness parameters, such as the average crushing force and specific energy absorption (SEA), were calculated using subsequent load–displacement relationships. The CHMC maintained a high level of structural integrity and post-crush performance, relative to traditional CF/epoxy. The influence of the curing time and volumetric ratios of the polyurea/epoxy dual-hybridized matrix system on the crashworthiness parameters was also investigated. The results reveal that the load carrying capacity and total energy absorption tend to increase with greater polyurea thickness and lower elapsed reaction curing time of the epoxy although this is typically a function of the loading rate. Finally, the mechanism by which the CHMC provides increased damage tolerance was also investigated using scanning electron microscopy (SEM).
تدمد: 1359-8368
DOI: 10.1016/j.compositesb.2014.10.053
URL الوصول: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c8e1a3b23d1ae8e9f6676d44762a8268
حقوق: OPEN
رقم الأكسشن: edsair.doi.dedup.....c8e1a3b23d1ae8e9f6676d44762a8268
قاعدة البيانات: OpenAIRE
الوصف
تدمد:13598368
DOI:10.1016/j.compositesb.2014.10.053