对称层合复合材料CNG储气罐的首层破坏压力

G. Shrigandhi, Mihil Shah, B. S. Kothavale
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引用次数: 0

摘要

近年来,压缩天然气(CNG)作为汽车燃料被过度发展,因为它比汽油和柴油燃料便宜且环保。为了提高燃油效率,使用轻质复合压力容器储罐来储存CNG。纤维增强复合材料由于具有较高的比强度,是目前应用最为广泛的材料。合成纤维如碳、玻璃纤维被用于制造这些压力容器。近几十年来,由于对环境的考虑,合成纤维与天然纤维的杂交得到了研究人员的关注。本文以蔡武破坏准则为基础,重点研究天然纤维的加入对首层破坏压力的影响。研究了碳/环氧纤维、e -玻璃/环氧纤维的层压顺序及其与abaca纤维的杂化。在其他天然纤维中,Abaca是最强的,因为它含有高纤维素,这是纤维强度的原因。考虑容量为30升,内径261mm,厚度12mm,两端封闭,施加压力为25mpa的CNG气罐。在不同的螺旋缠绕方向(θ = 15°、25°、35°、45°、55°、60°、75°)下,分析了对称层合材料的堆叠顺序[(90)2/ θ/(90)2]S。研究了一种厚度均匀的合成纤维和天然纤维混合管。对第一层破坏压力的模拟结果与理论结果进行了比较。欧特克Helius复合软件用于计算材料性能,首先,层失效分析。结果表明,破裂压力随螺旋角θ的增大而减小,且在[(90)2/岂能- 15°/(90)2]S的叠加序列中,破裂压力在所有管中均最大。与标准碳管相比,当缠绕角度在15°至45°之间时,混合碳/Abaca管的爆裂压力降低了69.5%至42%。对于混合E-Glass/Abaca管,与标准E-Glass管相比,当缠绕角度在15°至45°之间时,爆裂压力降低了21%至4.7%。对于混合碳/Abaca管,在55°~ 75°螺旋角范围内,与碳管相比,破裂压力下降幅度分别为23.7% ~ 1.74%。与仅使用E-Glass管相比,当螺旋角在55°至75°之间时,E-Glass/Abaca管的破裂压力略有提高(1.14%至7.5%)。对于E-Glass管,中间层可以用Abaca纤维代替。
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First-Ply Failure Pressure of Symmetric Laminated Hybrid Composite CNG Tank
In recent years, compressed natural gas (CNG) as a fuel for the automobile is overgrowing, as it is cheap and environmental friendly compared to gasoline and diesel fuel. To improve fuel efficiency, lightweight composite pressure vessel tanks are used for the storage of CNG. Due to high specific strength, fiber-reinforced composites are most widely used. Synthetic fibers like carbon, glass fiber are used for the fabrication of these pressure vessels. In the last few decades, due to environmental concerns, the hybridization of synthetic fiber with natural fiber has gained the attention of researchers. This paper focuses study on the effect of adding natural fiber on first ply failure (FPF) pressure based on the Tsai-Wu failure criterion. The laminate stacking sequence on first ply failure pressure for carbon/epoxy, E-glass/epoxy, and hybridization of these fibers with abaca fiber is studied. Abaca is strongest among other natural fibers as it contains high cellulose which is responsible for strength of the fiber. CNG tank with a 30-liter capacity, inside diameter 261mm, thickness 12 mm, applied pressure of 25 MPa with both ends closed is considered. Stacking sequence of symmetric laminate [(90)2/∓θ/(90)2]S, for different orientation of helical winding i.e. θ = 15°, 25°, 35°, 45°, 55°, 60°, 75° is analysed for these composite materials. A hybrid tube made of synthetic and natural fiber with uniform thickness is considered. The simulation results of the first ply failure pressure are compared with theoretical results. Autodesk Helius Composite software is used for calculating material properties and, first, ply failure analysis. It is observed that burst pressure decreases as helical angle θ increases, and for the stacking sequence of [(90)2/∓15°/(90)2]S burst pressure is maximum for all tubes. The Burst pressure of the hybrid carbon/Abaca tube reduces by 69.5% to 42% for winding angle between 15° to 45° compared to standard carbon tube. For hybrid E-Glass/Abaca tube, burst pressure reduction was 21% to 4.7% for winding angle between 15° to 45° compared to standard E-Glass tube. For hybrid Carbon/Abaca tube, the drop in burst pressure is less 23.7% to 1.74%, respectively, compared to carbon tube for helical angle in the range 55° to 75°. Slight improvement in burst pressure (1.14% to 7.5%) is observed for the helical angle between 55° to 75° in the case of a hybrid E-Glass/Abaca tube compared to the E-Glass tube only. For the E-Glass tube, intermediate lamina can be replaced by Abaca fiber.
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