Kevlar织物软壁包容环抗冲击数值仿真分析研究

针对机匣包容性问题,提出Kevlar平纹织物本构模型的拟合方法,分别采用单层壳、多层壳、层合壳三种有限元建模方式对Kevlar织物软壁包容环弹道冲击过程进行模拟,发展了机匣包容性仿真分析模型。结果表明,多层壳模型和层合壳模型的计算结果更准确,并且可以通过调节摩擦因子使仿真结果与试验结果更接近。在此基础上研究了撞击点位置和弹体入射姿态对弹体剩余速度的影响。结果表明:在较小偏移距离内,撞击点的位置对剩余速度的影响可以忽略不计;滚转角和俯仰角对剩余速度影响较小,而对于偏航角,当角度大于30°时,剩余速度会随着角度的增大明显呈下降趋势,且弹体出射姿态也会发生明显变化。     

Kevlar纤维层合板抗弹性能的数值模拟

采用Ansys/Ls-dyna建立了Kevlar纤维层合板的三维有限元模型,模拟了Kevlar纤维层合板的抗侵彻过程和抗弹性能,模拟结果与实验吻合较好,证明了模拟方法以及模型参数的合理性。在此基础上讨论了靶板的抗弹机理以及破坏方式,分析得到了随着靶板厚度的变化,抗弹性能会出现一个拐点,靶板破坏方式会发生变化,而在拐点之后,靶板厚度增加,靶板吸收能量减少,抗弹性能降低的结论。对某种特定弹体,存在一个合理的厚度匹配,以发挥Kevlar纤维层和板的抗弹性能。     

Kevlar纤维布/剪切增稠液复合材料制备及防刺性能

采用纳米SiO2和聚乙二醇(PEG200)制备不同SiO2质量浓度的剪切增稠液体(Shear Thickening Fluid,STF),并检测其流变性能;用落锤式冲击实验装置检测纯Kevlar纤维布和经STF浸渍的STF-Kevlar复合纤维布防刺性能。研究结果表明:不同SiO2质量浓度的STF均有剪切增稠现象,随着SiO2质量浓度升高,起始粘度增大,增稠现象越显著,而临界剪切速率基本不变;同层数的STF-Kevlar复合纤维布的防刺性能明显优于纯Kevlar纤维布,防刺性能随SiO2质量浓度的增加而提高。     

3D打印连续芳纶纤维/聚乳酸波纹夹层结构复合材料的压缩性能研究

以连续芳纶纤维(Kevlar)为增强体,热塑性聚乳酸(PLA)为基体,采用熔融沉积成型(FDM)工艺,设计并制备了一体成型的Kevlar/PLA波纹夹层结构复合材料。研究了Kevlar/PLA波纹夹层结构复合材料在压缩载荷下的断裂模式,分析了结构参数、工艺参数对试样的压缩性能和结构密度的影响。结果表明,随着芯层波纹数量的增加,试样的压缩性能与结构密度均呈增大趋势;随着芯层波纹高度的增大,试样的压缩强度先增大后减小,结构密度不断减小;随着打印层高的增大,试样中的纤维体积含量不断减少,试样的压缩强度略有下降。     

Sliding Wear of the Hybrid Kevlar/PTFE Fabric Reinforced Phenolic Composite Filled with Nano-titania

The Kevlar/polytetrafluroethylene(Kevlar/PTFE) fabric composite can be used as a self-lubricating liner of the self-lubricating bearing.Many types of nano-particles can improve the tribological performance of the polymer-based composite.Unfortunately,up to now,published work on the effect of nano-particles on the tribological performance of the fabric composite which can be used as a self-lubricating liner is quite scarce.Therefore,for the purpose of exploring a way to significantly improve the tribological performance of the fabric composite,the tribological performance of the Kevlar/PTFE fabric composite filled with nano-titania is evaluated by using the block-on-ring wear tester.The scanning electron microscopy is utilized to observe the morphologies of worn surfaces of the fabric composites and the counterparts.The tensile properties of the composites are evaluated on the universal material testing machine.The test results show that the addition of nano-titania at a proper mass fraction of the matrix resin improves the wear resistance and the tensile strength,decreases the friction coefficient,and makes the wear volume of the composite reach a relative steady state more quickly;plastic deformation and microcutting are important for the wear of the fabric composite;a lubricating layer is formed on the worn surface of the composite during sliding,and the lubricating layer is critical for the tribological performance of the composite;the formation and properties of the lubricating layer are influenced by the nano-titania particles.The proposed study on the effect of nano-titania on the tribological performance of the Kevlar/PTFE fabric composite,especially on the evolution of the worn surface of the composite,provides the basis for further understanding of the influence mechanism of the nano-particles on the tribological performance of the composite and explores a method of improving the tribological performance of the composite.     

带束层角度对轮胎印痕的影响

试验研究以锦纶帘线为胎体,以芳纶与锦纶的复合帘线为带束层的子午线轮胎,带束层角度对轮胎印痕的影响。试验结果表明：在同种条件下,随着轮胎带束层角度的变化,轮胎接地印痕、受力分布发生变化。     

破片侵彻陶瓷/芳纶复合装甲数值模拟

利用三维非线性动力有限元程序LS-DYNA,建立了破片侵彻陶瓷/芳纶复合材料装甲的有限元分析模型,描述了侵彻过程的物理和力学现象,得出了一些重要参量的变化规律,与破片侵彻相同面密度的均质装甲钢装甲进行了比较.陶瓷/芳纶复合装甲的抗侵彻能力要优于相同面密度的均质钢装甲.     

Self adhesion of short Kevlar fibre-thermoplastic polyurethane composite

The self adhesion behaviour of thermoplastic polyurethane (TPU) in itself and its composite with short Kevlar fibre with respect to contact time, temperature, pressure, and fibre loading has been studied. The adhesion strength showed two linear increments of different slopes with respect to the square root of time: with temperature and pressure of contact, the adhesion strength was improved. The maximum strength was obtained with 20 phr of short fibre in only one of the mating substrates in the peel test sample. The duration for wetting and diffusion was shifted to longer time intervals with fibres loaded in both the substrates.     

The interfacial shear strength of Kevlar fiber/epoxy composite measured by the microdroplet test

Epoxy chloropropane (ECP) grafting modification method was used for the surface treatment of Kevlar fiber to improve the interfacial adhesion of the Kevlar fiber reinforced epoxy composite. The surface characteristics of untreated and treated Kevlar fiber were characterized by Fourier transform infrared (FT‐IR) spectroscope. The interfacial shear strength between epoxy and Kevlar fiber was analyzed by measuring from microdroplet specimens adhered onto a single carbon fiber. Microdroplet specimens exhibited different results of the interfacial strength due to the Kevlar fiber surface treatment. The results showed that a larger shear stress concentration arose along the interface for the surface treated model than for the untreated one.     

Thermal aging of a blend of high‐performance fibers

The focus of this work is the study of the thermal aging of high‐performance fibers used in the making of fire protective garments. Accelerated thermal aging tests were carried out on fabric samples made up of a blend of Kevlar® (poly p‐phenylene terephthalamide) and PBI (poly benzimidazole) staple fibers, as well as on yarns pulled from this fabric, by means of exposure to elevated temperatures, comprised between 190°C and 320°C. All samples underwent loss of breaking force retention. The material thermal life, defined as the time required for the fibers to attain a 50% reduction of the original breaking force, ranged between a dozen of days at the lowest exposure temperature, to less than an hour at the highest. Breaking force data were fitted using the Arrhenius model following two different approaches, namely the extrapolated thermal life value and the shift factors yielded by the time‐temperature superposition (TTS). The Arrhenius model seemed to describe appropriately the overall aging process, as inferred from the excellent fit obtained when using both approaches, although activation energies provided from both approaches are different. To follow the chemical evolution of the material with thermal aging, Fourier‐transform infrared (FTIR) analyses were conducted. The qualitative analysis of the FTIR spectra showed little evidence of chemical changes between the aged and the nonaged samples, indicating either that the aging process carries on without significant modification of the chemical structure of the fibers, or that FTIR is not an appropriate method to spot such a modification. © 2009 Wiley Periodicals, Inc. J Appl Polym Sci, 2010