A simplified method for predicting burst pressure of type III filament-wound CFRP composite vessels considering the inhomogeneity of fiber packing

Harada, Shunsuke; Arai, Yasuhiko; Araki, Wakako; Iijima, Takafumi; Kurosawa, Akimoto; Ohbuchi, Tomoyuki; Sasaki, Noriyuki

doi:10.1016/j.compstruct.2018.02.011

Cited by 37 publications

(19 citation statements)

References 38 publications

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“…The curve shows two distinct slopes indicating the elastic and inelastic deformation during axial compression. Several other researchers also reported similar behavior [ 2 , 3 , 27 ].…”

Section: Resultssupporting

confidence: 64%

“…A simple trend was observed in the case of the cylindrical samples, as the winding angle increases, radial compression properties improve [ 2 , 3 , 4 ]. This can be attributed to the positioning of the fibers in the load bearing direction.…”

Section: Resultsmentioning

confidence: 99%

“…This technique is also used in axis-nonsymmetrical parts, like wind turbine blades, chassis in buses, etc. [ 2 , 3 ]. In this process, the continuous filaments are wound over a rotating mandrel in order to produce cylindrical profiles with advanced mechanical performance.…”

Section: Introductionmentioning

confidence: 99%

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Axial and Radial Compression Behavior of Composite Rocket Launcher Developed by Robotized Filament Winding: Simulation and Experimental Validation

et al. 2021

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The principal objective of the work is to compare among carbon-glass filament wound epoxy matrix hybrid composites with a different fiber ratio made by robotized winding processes and optimize the geometry suitable for the Rocket Propelled Grenade Launcher. ANSYS based finite element analysis was used to predict the axial as well as radial compression behavior. Experimental samples were developed by a robot-controlled filament winding process that was incorporated with continuous resin impregnation. The experimental samples were evaluated for the corresponding compressional properties. Filament wound tubular composite structures were developed by changing the sequence of stacking of hoop layers and helical layers, and also by changing the angle of wind of the helical layers while keeping the sequence constant. The samples were developed from carbon and glass filaments with different carbon proportions (0%, 25%, 50%, 75%, and 100%) and impregnated with epoxy resin. The compressional properties of the tubular composites that were prepared by filament winding were compared with the predicted axial and radial compressional properties from computational modelling using the finite element model. A very high correlation and relatively small prediction error was obtained.

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“…The curve shows two distinct slopes indicating the elastic and inelastic deformation during axial compression. Several other researchers also reported similar behavior [ 2 , 3 , 27 ].…”

Section: Resultssupporting

confidence: 64%

Section: Resultsmentioning

confidence: 99%

See 1 more Smart Citation

Axial and Radial Compression Behavior of Composite Rocket Launcher Developed by Robotized Filament Winding: Simulation and Experimental Validation

et al. 2021

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Section: Methodsmentioning

confidence: 99%

“…Filament winding of the GF/epoxy layer at the outermost helical layer of a pressure vessel is a common practice in the manufacturing of COPVs for increasing impact and corrosion resistance. 33,43,44 Winding configurations of manufactured vessels are summarized in Table 1. After the winding process, composite vessels were cured at 80 C for 2 h using a rotating shaft in a curing oven and post-cured at 120 C for 2 h.…”

Section: Manufacturing Of Composite Vessels Using Filament Windingmentioning

confidence: 99%

Investigation of interlayer hybridization effect on burst pressure performance of composite overwrapped pressure vessels with load-sharing metallic liner

Kangal

Kartav

Tanoğlu

et al. 2019

Journal of Composite Materials

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In this study, multi-layered composite overwrapped pressure vessels for high-pressure gaseous storage were designed, modeled by finite element method and manufactured by filament winding technique. 34CrMo4 steel was selected as a load-sharing metallic liner. Glass and carbon filaments were overwrapped on the liner with a winding angle of [±11°/90°2]3 to obtain fully overwrapped composite reinforced vessel with non-identical front and back dome endings. The vessels were loaded with increasing internal pressure up to the burst pressure level. The mechanical performances of pressure vessels, (i) fully overwrapped with glass fibers and (ii) with additional two carbon hoop layers on the cylindrical section, were investigated by both experimental and numerical approaches. In numerical approaches, finite element analysis was performed featuring a simple progressive damage model available in ANSYS software package for the composite section. The metal liner was modeled as elastic–plastic material. The results reveal that the finite element model provides a good correlation between experimental and numerical strain results for the vessels, together with the indication of the positive effect on radial deformation of the COPVs due to the composite interlayer hybridization. The constructed model was also able to predict experimental burst pressures within a range of 8%. However, the experimental and finite element analysis results showed that hybridization of hoop layers did not have any significant impact on the burst pressure performance of the vessels. This finding was attributed to the change of load-sharing capacity of composite layers due to the stiffness difference of carbon and glass fibers.

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A Review on Electric and Fuel Cell Vehicle Anatomy, Technology Evolution and Policy Drivers towards EVs and FCEVs Market Propagation

Chandran

Palanisamy

Benson

et al. 2021

The Chemical Record

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The transportation sector is the largest consumer of fossil fuels; making it a major producer of greenhouse gases. Due to declining fossil fuel reserves and increasingly stringent vehicle emission regulations globally, it is essential to shift to alternative energy sources. Economic and eco‐friendly fuel‐efficient hybrid, electric, and fuel cell vehicles are regarded as one of the best alternative solutions to cope with the government policies and to reduce the rise in global temperature caused by the automotive sector. Technological advancements in fuel cells, batteries, and chargers have further supported the development of electric vehicles. The major challenges of range and charging time in electric vehicles can be countered by range extension technology and developing all‐electric hybrid vehicles. In this review, a comprehensive study of different type of vehicles and their architectures are presented. Insights on energy storage devices and converters of electric vehicles currently in use were also provided. Furthermore, various fuel cell advancements and the technical challenges faced during the commercialization of fuel cell vehicles were highlighted.

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A simplified method for predicting burst pressure of type III filament-wound CFRP composite vessels considering the inhomogeneity of fiber packing

Cited by 37 publications

References 38 publications

Axial and Radial Compression Behavior of Composite Rocket Launcher Developed by Robotized Filament Winding: Simulation and Experimental Validation

Axial and Radial Compression Behavior of Composite Rocket Launcher Developed by Robotized Filament Winding: Simulation and Experimental Validation

Investigation of interlayer hybridization effect on burst pressure performance of composite overwrapped pressure vessels with load-sharing metallic liner

A Review on Electric and Fuel Cell Vehicle Anatomy, Technology Evolution and Policy Drivers towards EVs and FCEVs Market Propagation

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