Behavior of Pull-Out and Movement Mechanisms of High-Performance Plain Weave Fabric Yarns

doi:10.16183/j.cnki.jsjtu.2020.419

Abstract

Abstract:

In order to study the movement mechanisms of plain weave fabric yarns, the numerical simulation of behavior of yarn pull-out and movement under various loading conditions was carried out on a typical plain-woven fabric. The effects of friction coefficients, model size, and pre-stress levels on yarn movement responses were analyzed in detail, and the coupling relation among pull-out length, pull-out fractured strength, and model parameter conditions, including friction coefficients and pre-stress levels were shown. The results indicate that positive correlations exist between peak pull-out loads and those main model parameters of plain weave fabrics, including the friction coefficients, model size, and pre-stress levels. As the pre-stress level rises from 200 MPa to 700 MPa, the peak pull-out load increases by 34.49%, and the existence of yarn crimps could lead to improvement of the pull-out loads. The pull-out fractured strength of yarns gradually increases with the growths of pre-stress levels and friction coefficients in the plain weave fabrics. Specifically, the pull-out fractured strength of yarns increases by 16.48% as the friction coefficient grow from 0.1 to 0.2. In addition, the pull-out fractured length of yarns of the plain-woven fabrics is highly dependent on the actual stress state, and the homogenization of the stress state is an important factor that influences the pull-out fractured length.

Key words: plain weave fabrics, yarn pull-out, movement, breakage, friction coefficient

CLC Number:

TU502

CHEN Jianwen, WU Shanxiang, ZHANG Ruonan, CHEN Wujun, FAN Jin, WANG Mingyang. Behavior of Pull-Out and Movement Mechanisms of High-Performance Plain Weave Fabric Yarns[J]. Journal of Shanghai Jiao Tong University, 2022, 56(4): 464-473.

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References 25

[1]	TABIEI A, NILAKANTAN G. Ballistic impact of dry woven fabric composites: A review[J]. Applied Mechanics Reviews, 2008, 61(1): 010801. doi: 10.1115/1.2821711 URL
[2]	陈晓钢. 纺织基防弹防穿刺材料的研究回顾[J]. 纺织学报, 2019, 40(6): 159-165.
	CHEN Xiaogang. Trend of research in textile-based protective materials against ballistic and stabbing[J]. Journal of Textile Research, 2019, 40(6): 159-165.
[3]	谢婉晨. 三维机织物复合材料头盔壳体的制备及成型[D]. 武汉: 武汉纺织大学, 2017.
	XIE Wanchen. Study on the preparation and forming of the helmet shell with composite materials of 3D woven fabric[D]. Wuhan: Wuhan Textile University, 2017.
[4]	何业茂. 高性能纤维增强树脂基复合材料防弹装甲的研究[D]. 天津: 天津工业大学, 2017.
	HE Yemao. Research on bulletproof armor of high-performance reinforced resin matrix composite[D]. Tianjin: Tianjin Polytechnic University, 2017.
[5]	裴鹏英, 胡雨, 胡慧娜, 等. 柔性防弹防刺服开发关键技术[J]. 纺织导报, 2017, 10: 62-65.
	PEI Pengying, HU Yu, HU Huina, et al. Key technologies for developing flexible bullet-proof/stabresistant body armor[J]. China Textile Leader, 2017, 10: 62-65.
[6]	王彦广, 李健全, 李勇, 等. 近空间飞行器的特点及其应用前景[J]. 航天器工程, 2007, 16(1): 50-57.
	WANG Yanguang, LI Jianquan, LI Yong, et al. Characters and application prospects of near space flying vehicles[J]. Spacecraft Engineering, 2007, 16(1): 50-57.
[7]	顾正铭. 平流层飞艇蒙皮材料的研究[J]. 航天返回与遥感, 2007, 28(1): 62-66.
	GU Zhengming. Research of stratospheric airships’ skin material[J]. Spacecraft Recovery & Remote Sensing, 2007, 28(1): 62-66.
[8]	NILAKANTAN G, GILLESPIE J W. Ballistic impact modeling of woven fabrics considering yarn strength, friction, projectile impact location, and fabric boundary condition effects[J]. Composite Structures, 2012, 94(12): 3624-3634. doi: 10.1016/j.compstruct.2012.05.030 URL
[9]	PAN N, YOON M Y. Behavior of yarn pullout from woven fabrics: Theoretical and experimental[J]. Textile Research Journal, 1993, 63(11): 629-637. doi: 10.1177/004051759306301103 URL
[10]	DONG Z X, SUN C T. Testing and modeling of yarn pull-out in plain woven Kevlar fabrics[J]. Composites Part A: Applied Science and Manufacturing, 2009, 40(12): 1863-1869. doi: 10.1016/j.compositesa.2009.04.019 URL
[11]	YANG Y F, CHEN X G. Investigation on energy absorption efficiency of each layer in ballistic armour panel for applications in hybrid design[J]. Composite Structures, 2017, 164: 1-9. doi: 10.1016/j.compstruct.2016.12.057 URL
[12]	NILAKANTAN G, MERRILL R L, KEEFE M, et al. Experimental investigation of the role of frictional yarn pull-out and windowing on the probabilistic impact response of Kevlar fabrics[J]. Composites Part B: Engineering, 2015, 68: 215-229. doi: 10.1016/j.compositesb.2014.08.033 URL
[13]	WANG Y Q, MIAO Y Y, HUANG L J, et al. Effect of the inter-fiber friction on fiber damage propagation and ballistic limit of 2-D woven fabrics under a fully confined boundary condition[J]. International Journal of Impact Engineering, 2016, 97: 66-78. doi: 10.1016/j.ijimpeng.2016.06.007 URL
[14]	HASANZADEH M, MOTTAGHITALAB V, BABAEI H, et al. The influence of carbon nanotubes on quasi-static puncture resistance and yarn pull-out behavior of shear-thickening fluids (STFs) impregnated woven fabrics[J]. Composites Part A: Applied Science and Manufacturing, 2016, 88: 263-271. doi: 10.1016/j.compositesa.2016.06.006 URL
[15]	SEBASTIAN S A, BAILEY A I, BRISCOE B J, et al. Effect of a softening agent on yarn pull-out force of a plain weave fabric[J]. Textile Research Journal, 1986, 56(10): 604-611. doi: 10.1177/004051758605601003 URL
[16]	SEBASTIAN S D, BAILEY A I, BRISCOE B J, et al. Extensions, displacements and forces associated with pulling a single yarn from a fabric[J]. Journal of Physics D: Applied Physics, 1987, 20(1): 130-139. doi: 10.1088/0022-3727/20/1/020 URL
[17]	MOTAMEDI F, BAILEY A I, BRISCOE B J, et al. Theory and practice of localized fabric deformations[J]. Textile Research Journal, 1989, 59(3): 160-172. doi: 10.1177/004051758905900305 URL
[18]	MARTÍNEZ M A, NAVARRO C, CORTÉS R, et al. Friction and wear behaviour of Kevlar fabrics[J]. Journal of Materials Science, 1993, 28(5): 1305-1311. doi: 10.1007/BF01191969 URL
[19]	BAZHENOV S. Dissipation of energy by bulletproof aramid fabric[J]. Journal of Materials Science, 1997, 32(15): 4167-4173. doi: 10.1023/A:1018674528993 URL
[20]	NILAKANTAN G, GILLESPIE J W . Yarn pull-out behavior of plain woven Kevlar fabrics: Effect of yarn sizing, pullout rate, and fabric pre-tension[J]. Composite Structures, 2013, 101: 215-224. doi: 10.1016/j.compstruct.2013.02.018 URL
[21]	BILISIK K, YILDIRIM B. Properties of stick-slip stage of yarn pull-out in Para-aramid woven fabric[J]. Fibers and Polymers, 2013, 14(4): 630-638. doi: 10.1007/s12221-013-0630-5 URL
[22]	YANG Y F, CHEN X G. Investigation of failure modes and influence on ballistic performance of ultra-high molecular weight polyethylene (UHMWPE) uni-directional laminate for hybrid design[J]. Composite Structures, 2017, 174: 233-243. doi: 10.1016/j.compstruct.2017.04.033 URL
[23]	李帅, 陈永霖, 肖畅, 等. 平流层飞艇蒙皮复合织物材料撕裂性能研究[J]. 合肥工业大学学报, 2020, 43(11): 1456-1462.
	LI Shuai, CHEN Yonglin, XIAO Chang, et al. Study on tear properties of composite fabric materials for stratospheric airship envelope[J]. Journal of Hefei University of Technology, 2020, 43(11): 1456-1462.
[24]	朱德举, 欧云福. 标距和应变率对Kevlar 49单束拉伸力学性能的影响[J]. 复合材料学报, 2016, 33(2): 225-233.
	ZHU Deju, OU Yunfu. Effects of gauge length and strain rate on tensile mechanical properties of Kevlar 49 single yarn[J]. Acta Materiae Compositae Sinica, 2016, 33(2): 225-233.
[25]	ZHU D J, SORANAKOM C, MOBASHER B, et al. Experimental study and modeling of single yarn pull-out behavior of Kevlar© 49 fabric[J]. Composites Part A: Applied Science and Manufacturing, 2011, 42(7): 868-879. doi: 10.1016/j.compositesa.2011.03.017 URL

方向	椭圆截面/mm		路径参数/mm
方向	长半轴	短半轴	周期	幅值
经纱	0.655	0.155	2.997	0.122
纬纱	0.585	0.139	2.982	0.096

工况	F/MPa	Z/mm	u
I	0	15	0、 0.1、 0.2
II	200、300、400、 500、600、700	15	0.2
III	40、60、80、 100、120	15	0、 0.1、0.2