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Vectran纤维在飞艇蒙皮材料中的力学性能研究 被引量:2

The study on the performance and application of Vectran in airship envelope materials
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摘要 为了研究Vectran纱线是否符合飞艇蒙皮材料的性能要求,探究捻度对Vectran长丝纱的力学性能的影响,并织造Vectran平纹织物。通过比较四种不同的Vectran织物的拉伸、撕裂性能,讨论涂层对Vectran织物力学性能的影响以及不同的撕裂失效模式。结果表明:加捻可以增强Vectran长丝纱的断裂强力,但需要特殊工艺,随着捻度增加,强力出现先降低后增加再降低的趋势;成本更低的400D Vectran织物可以达到飞艇蒙皮材料的力学性能要求;Vectran涂层织物与未涂层织物的撕裂失效模式不同。 In order to study whether a Vectran fiber can be made into a fabric that meets the performance requirements of airship envelope material, the mechanical properties of the yarn and fabric were tested respectively. Firstly, the effect of twist on mechanical properties of Vectran filament yarn was investigated by breaking strength test and data fitting. The results show that twisting can enhance the breaking strength of Vectran filament yarn, but special twisting technology is needed. As the twist increases, the strength decreases first, then increases and then decreases. Additionally, by comparing the tensile and tearing properties of four different Vectran fabrics, the influence of coating on the mechanical properties of Vectran fabrics was discussed. The results show that the 400 D Vectran fabric can meet the mechanical properties of the airship envelope material and has the advantage of lower cost. The tear failure mode of Vectran coated fabrics is different from that of uncoated fabrics.
作者 崔馨文 蒋金华 李俊 CUI Xin-wen;JIANG Jin-hua;LI Ju(College of Fashion&Design,Donghua University,Shanghai 200051,China;College of Textile,Donghua University,Shanghai 201620,China;Key Laboratory of Clothing Design and Technology,Ministry of Education,Donghua University,Shanghai 200051,China)
出处 《复合材料科学与工程》 CAS 北大核心 2022年第1期73-78,共6页 Composites Science and Engineering
基金 中央高校基本科研业务费专项基金(2232021G-08)。
关键词 平流层飞艇 承力层织物 Vectran纤维 力学性能 复合材料 stratospheric airship load-bearing fabric Vectran fiber mechanical properties composites
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