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Multilayered and Multidirectionally-stitched aramid Woven Fabric Structures: Experimental Characterization of Ballistic Performance by Considering the Yarn Pull-out Test

机译:多层和多方向缝制的芳族聚酰胺机织织物结构:考虑纱线拉伸试验的弹道性能的实验表征

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Abstract The aim of this study was to understand the energy absorption mechanism and failure modes of newly developed multidirectionallystitched structures. Para-aramid woven fabric was used. The structures were in unstitched and stitched forms. Nylon 6.6 yarn was used to stitch the structure in one, two and four directions whereas Kevlar® 129 yarn was used to make only the four-directionally-stitched structures. The yarn pull-out fixture was developed and the yarn pullout test was performed on single woven fabric and stitched structures. Ballistic tests were performed on the structures using 9 mm full metal jacketed projectiles with a speed of 300 to 400 m/s. If the applied kinetic energy level is under the yarn breaking extension, crimp in the orthogonal yarns at the fabric structure is firstly removed, and thereafter yarn pull-out takes place in the structure plane, and later stage fabric deformation occurs in the out-of-plane direction of the structure. This phenomenon continues from the outside to the inside layers. If the applied kinetic energy level is above the yarn breaking extension, firstly partial and total filament breakages and subsequently crimp removal and yarn pull out stages occur. These phenomena take place as multiple yarn failure in the outer layers and mostly crimp removal and yarn pull-out towards the inside layers occur. In both cases, fabric and structure bending were ignored. The energy absorption level of the stitched structures was slightly higher than that of the unstitched structures due to the fact that some of the energy was absorbed to delaminate the interlayer, which was locked by the stitching yarns. Also, the conical depth in the stitched structure was low compared with that of the unstitched structure.
机译:摘要本研究的目的是了解新型多向缝制结构的能量吸收机理和破坏模式。使用对位芳族聚酰胺机织织物。结构为未缝合和缝合形式。尼龙6.6纱线用于在一个,两个和四个方向上缝合结构,而凯夫拉尔129纱线仅用于制造四方向缝合的结构。开发出纱线抽出夹具,并在单机织物和缝合结构上进行了纱线抽出测试。使用9毫米全金属护套射弹以300至400 m / s的速度对结构进行弹道测试。如果施加的动能水平在断纱伸长量以下,则首先消除织物结构上正交纱线中的卷曲,然后在结构平面内拉出纱线,随后阶段织物变形发生在纱线外。结构的平面方向。这种现象从外层一直延伸到内层。如果所施加的动能水平高于断头伸长率,则首先发生部分和全部长丝断裂,然后发生卷曲去除和纱线拔出阶段。这些现象是由于外层多次出现纱线故障而发生的,主要是去除了卷曲并向内层拉出了纱线。在这两种情况下,织物和结构的弯曲都被忽略。缝合结构的能量吸收水平比未缝合结构的能量吸收水平略高,这是由于以下事实:吸收了一些能量以使中间层分层,该中间层被缝合纱线锁定。另外,与未缝合结构相比,缝合结构中的圆锥深度低。

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