This article presents a study of the effect of through-the-thickness stitching yarns upon the strength and failure behavior of multidirectionally reinforced composites. The in-plane yarns were placed in four directions (0, Ϯ45, 90) to form a quasi-isotropic preform, which had open spaces between adjacent yarns. These interyarn spaces allowed easy insertion of the through-the-thickness stitching yarns without significant damage of the in-plane fibers. Fiber volume fractions of over 54 pct were obtained by this method. The through-the-thickness yarn sizes used in this study were 2, 4, and 6 kilo-filament (kf). Non-stitched preforms were also manufactured with the same fiber content and by the same procedure as the stitched preforms for the control experiments. All preforms were infiltrated with epoxy resin by the resin transfer molding (RTM) technique. In-plane tensile and compressive strength, interlaminar shear strength, and mode I fracture toughness of the carbon/epoxy composites were measured at three through-the-thickness yarn contents. Although the through-the-thickness yarns significantly enhanced the mode I fracture toughness, they tended to degrade the in-plane tensile and compressive strength. The failure process under interlaminar shear loading by double notch shear tests showed two distinct stages: the fiber-matrix interfacial failure followed by the breakage/debonding of the through-the-thickness yarns. The through-the-thickness yarns caused a reduction of the initial failure load in the first stage but could enhance the final failure load in the second stage. In composites with 6 kf through-the-thickness yarns, the final failure load could exceed the initial failure load. Scanning electron microscope (SEM) and optical microscopic examinations were also conducted for observing the failure mechanisms and fracture surfaces.
This article presents a study of the effect of through-the-thickness stitching yarns upon the strength and failure behavior of multidirectionally reinforced composites. The in-plane yarns were placed in four directions (0, Ϯ45, 90) to form a quasi-isotropic preform, which had open spaces between adjacent yarns. These interyarn spaces allowed easy insertion of the through-the-thickness stitching yarns without significant damage of the in-plane fibers. Fiber volume fractions of over 54 pct were obtained by this method. The through-the-thickness yarn sizes used in this study were 2, 4, and 6 kilo-filament (kf). Non-stitched preforms were also manufactured with the same fiber content and by the same procedure as the stitched preforms for the control experiments. All preforms were infiltrated with epoxy resin by the resin transfer molding (RTM) technique. In-plane tensile and compressive strength, interlaminar shear strength, and mode I fracture toughness of the carbon/epoxy composites were measured at three through-the-thickness yarn contents. Although the through-the-thickness yarns significantly enhanced the mode I fracture toughness, they tended to degrade the in-plane tensile and compressive strength. The failure process under interlaminar shear loading by double notch shear tests showed two distinct stages: the fiber-matrix interfacial failure followed by the breakage/debonding of the through-the-thickness yarns. The through-the-thickness yarns caused a reduction of the initial failure load in the first stage but could enhance the final failure load in the second stage. In composites with 6 kf through-the-thickness yarns, the final failure load could exceed the initial failure load. Scanning electron microscope (SEM) and optical microscopic examinations were also conducted for observing the failure mechanisms and fracture surfaces.
By reviewing the design methodology of textile structural composites, the relationship between the various textile forming techniques and some basic structural elements under various loading configurations is detailed. Additionally, an analytical technique to predict the stiffnesses of the resulting textile composite is discussed and a comparison between the predicted and measured in-plane stiffnesses for three different textile architectures is reviewed. Finally, an examination is made of the Mode I fracture toughness characterization of a stitched textile composite.
scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.
hi@scite.ai
10624 S. Eastern Ave., Ste. A-614
Henderson, NV 89052, USA
Copyright © 2024 scite LLC. All rights reserved.
Made with 💙 for researchers
Part of the Research Solutions Family.