2018
DOI: 10.1007/s10853-018-2481-3
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Tensile strength, peel load, and static puncture resistance of laminated composites reinforced with nonwoven fabric

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Cited by 7 publications
(5 citation statements)
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“…This outcome suggests that the defect of symmetrical multiple delaminations may result in a decrease in the stiffness of composite [19,20]. Furthermore, the slope in stage I, II and III of Specimen B successively decreases with bending load increasing, which shows that the resistance to deformation when the structure is under stress becomes [21,22]. From a macro perspective, the catastrophic failure of specimen without defects is explosive but the instability failure of specimen containing symmetrical multiple delaminations is intermittent.…”
Section: Effects Of Delaminations On Damage Evolution Of Specimensmentioning
confidence: 95%
“…This outcome suggests that the defect of symmetrical multiple delaminations may result in a decrease in the stiffness of composite [19,20]. Furthermore, the slope in stage I, II and III of Specimen B successively decreases with bending load increasing, which shows that the resistance to deformation when the structure is under stress becomes [21,22]. From a macro perspective, the catastrophic failure of specimen without defects is explosive but the instability failure of specimen containing symmetrical multiple delaminations is intermittent.…”
Section: Effects Of Delaminations On Damage Evolution Of Specimensmentioning
confidence: 95%
“…Regardless of the random combination of needle punching rate and needle punching depth, all load–displacement curves exhibit three creeps, indicating the failure of the top TPU sheet, nonwoven interlayer, and bottom TPU sheet in order.
Figure 13.(a) Schematic diagrams of laminated composites; (b) b 1 The nonwovenlayer, b 2 needle punching mechanism, and b 3 the lamination structure of the laminated composite and b 4 the needle punching machine; (c) Adhesion mechanism of LMPET fibers: c 1 melting-and-bonding diagram and c 2 thermal bonding point; (d) Image of entangled fibers of the core layer in the laminated composites (200-15) where Kevlar fibers are marked in yellow and LMPET fibers are marked in blue. 75 LMPET: low-melting-point polyester.
…”
Section: Compositionmentioning
confidence: 99%
“…In addition to the fabric can be compounded with each other, the sheet and fabric can be thermally bonded to form composite materials. Lin et al 75 used Kevlar/LMPET 74 nonwoven interlayer and two TPU covers to form the laminated composites via thermal bonding which is shown in Figure 13. Results show that tensile strength and static puncture resistance mainly depend on the needle punching depth to a large extent, primarily on the tangled fiber points.…”
Section: Compositionmentioning
confidence: 99%
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“…On the other hand, the coating endows excellent mechanical strength and protective properties, and the chemically cross-linked organic component effectively hinders crack propagation . Furthermore, adjusting parameters such as nanofiller content, , particle size, , and ratios in the coating solution and silk cocoon-like layer structure can substantially improve the puncture resistance of the composites. Moreover, with the advancement of industrialization and the development of the chemical field, the significance of protective materials possessing outstanding resistance to strong acids and bases cannot be overstated.…”
Section: Introductionmentioning
confidence: 99%