Abstract:The aim of this study was to improve four-point bending performance of foam core sandwich composite beams by applying various core machining configurations. Sandwich composites have been manufactured using perforated and grooved foam cores by vacuum-assisted resin transfer moulding method with vinyl-ester resin system. The influence of grooves and perforations on the mechanical performance of marine sandwich composite beams was investigated under four-point bending test considering the weight gain. Bending str… Show more
“…Load versus crosshead displacement curves of the sandwich specimens with different support spans tested under 3PB and 4PB tests are shown in Figure 2, Figure 3, Figure 4, Figure 5 and Figure 6. All results are also summarised in Table 4, including the initial bending stiffness (K i ), ultimate bending strength (P u ), ultimate bending strength to weight ratio (P u /W), analytical to experimental ultimate bending load ratio (P a /P u ), equivalent bending to effective bending ratio (E eq./ E eff ) and failure modes (related analytical formulations were presented in detail in a previous study 48 ). The analytical loads (P a ) for the sandwich beams were determined using simple beam theory using the mechanical properties of the E-glass/vinyl ester face sheet and PVC foam materials.…”
Section: Resultsmentioning
confidence: 99%
“…was determined using the deflection formula obtained from the experimental results for sandwich beams. 9,15,21,48 …”
This paper presents a rigorous study on the flexural behaviour of symmetric and asymmetric marine sandwich beams consisting of polyvinyl chloride (PVC) foam core and glass fibre composite face-sheets. The sandwich beams have a shear-span-to depth ratio (a/d) ranging from 2 to 7.5 and loaded under three- and four-point static bending configurations. The effect of mid-plane asymmetry, stacking sequence, fabric weight, and core type on the failure mode, bending rigidity and strength of the sandwich composites were investigated. Two-way analysis of variance (ANOVA) analysis indicated that the effect of the a/d ratio and the loading type had a similar effect on failure load. The a/d ratio had a greater influence on the initial bending stiffness than the loading type for the asymmetric beams.
“…Load versus crosshead displacement curves of the sandwich specimens with different support spans tested under 3PB and 4PB tests are shown in Figure 2, Figure 3, Figure 4, Figure 5 and Figure 6. All results are also summarised in Table 4, including the initial bending stiffness (K i ), ultimate bending strength (P u ), ultimate bending strength to weight ratio (P u /W), analytical to experimental ultimate bending load ratio (P a /P u ), equivalent bending to effective bending ratio (E eq./ E eff ) and failure modes (related analytical formulations were presented in detail in a previous study 48 ). The analytical loads (P a ) for the sandwich beams were determined using simple beam theory using the mechanical properties of the E-glass/vinyl ester face sheet and PVC foam materials.…”
Section: Resultsmentioning
confidence: 99%
“…was determined using the deflection formula obtained from the experimental results for sandwich beams. 9,15,21,48 …”
This paper presents a rigorous study on the flexural behaviour of symmetric and asymmetric marine sandwich beams consisting of polyvinyl chloride (PVC) foam core and glass fibre composite face-sheets. The sandwich beams have a shear-span-to depth ratio (a/d) ranging from 2 to 7.5 and loaded under three- and four-point static bending configurations. The effect of mid-plane asymmetry, stacking sequence, fabric weight, and core type on the failure mode, bending rigidity and strength of the sandwich composites were investigated. Two-way analysis of variance (ANOVA) analysis indicated that the effect of the a/d ratio and the loading type had a similar effect on failure load. The a/d ratio had a greater influence on the initial bending stiffness than the loading type for the asymmetric beams.
“…The price of the foam and epoxy resin are 852.00 $/m 3 and 4662.71 $/m 3 , respectively. A typical thickness of 25 mm, which was commonly adopted in [15,19,22,23,26], was decided as the target thickness of the foam for evaluating the cost of infused cores. The fractions of infused resin were 0.00%, 1.08%, and 6.20% in volume for the plain, GP, and GPC cores, respectively.…”
Section: Cost Evaluationmentioning
confidence: 99%
“…Balıko glu et al [26] investigated the effect of perforated and grooved foam core modification on the bending performance of composite sandwich beams made of E-glass fibre/vinylester resin composite face sheets and closed cell PVC foam. The experimental results showed that the bending strength and effective stiffness of sandwich beam increased by 34% and 61%, respectively, compared with that without core modification.…”
Composite sandwich structures are widely used in the fields of aviation, marine, and energy due to their high specific stiffness and design flexibility. Improving the mechanical properties of the cores is significant to the strength, modulus, and stability of composite sandwich structures. Two kinds of core machining configurations were designed by combining thin grooves, perforated holes, and thick contour cuts as well as non-machining plain cores. The cores and sandwich structures with these configurations were fabricated using a vacuum-assistant infusion process. Static tensile, compressive, shear, and peeling tests were conducted on the infused cores and sandwich structures. The results showed that the tensile, compressive, and shear moduli, and compressive strength of the infused cores can be greatly improved. The tensile strength changed negligibly due to stress concentration induced by irregular foam cell and the shear-lag phenomenon of the resin column/foam interface. The shear strength of the infused cores increased slightly. The thick contour cuts and perforated holes can greatly improve the face sheet/core peel capacity of the sandwich structures, whereas the thin grooves can moderately improve the peel capacity. Both infused cores with the designed machining configurations exhibited positive effects on the compressive, tensile, and shear moduli, and compressive strength, considering the material costs. The study provides a comprehensive and quantitative insight into the effects of core machining configurations on mechanical properties of infused cores and composite sandwich structures.
“…The final composition of a sandwich structure depends on the target application. For example, polymer foam cores are generally used in car flooring, boat parts, as well as turbine blades, as they have good rigidity, high strength, and resistance to fatigue and temperature [ 12 , 13 , 14 , 15 ]. Feng and Aymerich [ 13 ] studied the effect of the density of a polyvinyl chloride (PVC) foam core on sandwich panels with carbon/epoxy-laminated facings, resulting in a composite structure with excellent stiffness.…”
This work focuses on the manufacturing and characterization of highly environmentally friendly lightweight sandwich structures based on polylactide (PLA) honeycomb cores and PLA-flax fabric laminate skins or facings. PLA honeycombs were manufactured using PLA sheets with different thicknesses ranging from 50 to 500 μm. The PLA sheets were shaped into semi-hexagonal profiles by hot-compression molding. After this stage, the different semi-hexagonal sheets were bonded together to give hexagonal panels. The skins were manufactured by hot-compression molding by stacking two Biotex flax/PLA fabrics with 40 wt% PLA fibers. The combined use of temperature (200 °C), pressure, and time (2 min) allowed PLA fibers to melt, flow, and fully embed the flax fabrics, thus leading to thin composite laminates to be used as skins. Sandwich structures were finally obtained by bonding the PLA honeycomb core with the PLA-flax skins using an epoxy adhesive. A thin PLA nonwoven was previously attached to the external hexagonal PLA core, to promote mechanical interlock between the core and the skins. The influence of the honeycomb core thickness on the final flexural and compression properties was analyzed. The obtained results indicate that the core thickness has a great influence on the flexural properties, which increases with core thickness; nevertheless, as expected, the bonding between the PLA honeycomb core and the skins is critical. Excellent results have been obtained with 10 and 20 mm thickness honeycombs with a core shear of about 0.60 and facing bending stresses of 31–33 MPa, which can be considered as candidates for technical applications. The ultimate load to the sample weight ratio reached values of 141.5 N·g−1 for composites with 20 mm thick PLA honeycombs, which is comparable to other technical composite sandwich structures. The bonding between the core and the skins is critical as poor adhesion does not allow load transfer and, while the procedure showed in this research gives interesting results, new developments are necessary to obtain standard properties on sandwich structures.
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