Naval Architecture, Ocean and Civil Engineering

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

Expand
  • 1. School of Science, Nanjing University of Science and Technology, Nanjing 210094, China
    2. Space Structures Research Center, Shanghai Jiao Tong University, Shanghai 200030,China
    3. Engineering Institute of Corps of Engineers, Army Engineering University of PLA, Nanjing 210007, China

Received date: 2020-12-09

  Online published: 2022-05-07

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.

Cite this article

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 Jiaotong University, 2022 , 56(4) : 464 -473 . DOI: 10.16183/j.cnki.jsjtu.2020.419

References

[1] TABIEI A, NILAKANTAN G. Ballistic impact of dry woven fabric composites: A review[J]. Applied Mechanics Reviews, 2008, 61(1): 010801.
[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.
[2] 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.
[3] 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.
[4] 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.
[5] 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.
[6] 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.
[7] 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.
[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.
[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.
[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.
[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.
[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.
[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.
[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.
[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.
[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.
[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.
[19] BAZHENOV S. Dissipation of energy by bulletproof aramid fabric[J]. Journal of Materials Science, 1997, 32(15): 4167-4173.
[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.
[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.
[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.
[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.
[23] 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.
[24] 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.
Outlines

/