Roszak Maciej, Pyka Dariusz, Bocian Mirosław, Barsan Narcis, Dragašius Egidijus, Jamroziak Krzysztof
Department of Mechanics, Materials Science and Biomedical Engineering, Wrocław University of Science and Technology, Smoluchowskiego 25, 50-370 Wrocław, Poland.
Department of Environmental Engineering and Mechanical Engineering, Vasile Alecsandri University of Bacau, Calea Marasesti 157, 600115 Bacau, Romania.
Polymers (Basel). 2023 Aug 29;15(17):3584. doi: 10.3390/polym15173584.
Multi-layer fabrics are commonly used in ballistics shields with a lower bulletproof class to protect against pistol and revolver bullets. In order to additionally limit the dynamic deflection of the samples, layers reinforced with additional materials, including non-Newtonian fluids compacted by shear, are additionally used. Performing a wide range of tests in each case can be very problematic; therefore, there are many calculation methods that allow, with better or worse results, mapping of the behavior of the material in the case of impact loads. The search for simplified methods is very important in order to simplify the complexity of numerical fabric models while maintaining the accuracy of the results obtained. In this article, multi-layer composites were tested. Two samples were included in the elements subjected to shelling. In the first sample, the outer layers consisted of aramid fabrics in a laminate with a thermoplastic polymer matrix. The middle layer contained a non-Newtonian shear-thickening fluid enclosed in hexagonal (honeycomb) cells. The fluid was produced using polypropylene glycol and colloidal silica powder with a diameter of 14 µm in the proportions of 60/40. The backing plate was made using a 12-layer composite made of Twaron para-aramid fabrics with a DCPD matrix-not yet used in a wide range of ballistics. Then, numerical simulations were carried out in the Abaqus/Explicit dynamic analysis. The Johnson-Cook constitutive strength model was used to describe the behavior of elastic-plastic materials constituting the elements of the projectiles. For the non-Newtonian fluid, a Up-Us EOS was used. The inner layers of the fabric were treated as an orthotropic material. Complete homogenization of the sample layers was carried out, thanks to which each layer was treated as a homogeneous continuum. As a parameter of fracture mechanics for shield components, the strain criterion was used with the smooth particles hydrodynamics method (SPH). Then, the results of simulations were compared with the results of the ballistic test for both samples placed next to each other, which resulted in the formation of a multi-layer composite in one ballistic test subjected to impact loads during firing with a 9 × 19 mm Parabellum FMJ projectile with an initial velocity of 370 ± 10 m/s. The results of numerical tests are very similar to the ballistic tests, which indicates the correct mapping of the process and the correct conduct of layer homogenization. The applied proportions of the components in the non-Newtonian fluid allowed a reduction in the deflection compared to previous studies. Additionally, the proposal to use a DCPD matrix allowed to obtain a much lower deflection value compared to other materials, which is a novelty in the field of production of ballistic shields.
多层织物常用于防弹等级较低的防弹盾牌中,以抵御手枪和左轮手枪子弹。为了进一步限制样品的动态挠度,还使用了用包括剪切压实的非牛顿流体在内的附加材料增强的层。在每种情况下进行广泛的测试可能非常困难;因此,有许多计算方法可以或多或少准确地模拟材料在冲击载荷情况下的行为。寻找简化方法非常重要,以便在保持所得结果准确性的同时简化数值织物模型的复杂性。在本文中,对多层复合材料进行了测试。在经受炮击的元件中包括两个样品。在第一个样品中,外层由芳纶织物与热塑性聚合物基体组成的层压板构成。中间层包含封闭在六边形(蜂窝状)单元中的非牛顿剪切增稠流体。该流体是使用聚丙二醇和直径为14 µm的胶体二氧化硅粉末按60/40的比例制成的。背板是用由Twaron对位芳纶织物与DCPD基体组成的12层复合材料制成的——尚未在广泛的弹道学中使用。然后,在Abaqus/Explicit动态分析中进行了数值模拟。使用Johnson-Cook本构强度模型来描述构成弹丸元件的弹塑性材料的行为。对于非牛顿流体,使用了Up-Us状态方程。织物的内层被视为正交各向异性材料。对样品层进行了完全均匀化处理,因此每层都被视为均匀连续体。作为盾牌部件断裂力学的一个参数,应变准则与光滑粒子流体动力学方法(SPH)一起使用。然后,将模拟结果与并排放置的两个样品的弹道测试结果进行比较,这导致在一次弹道测试中形成了多层复合材料,该测试在发射9×19毫米帕拉贝鲁姆全金属被甲弹时承受冲击载荷,初始速度为370±10米/秒。数值测试结果与弹道测试结果非常相似,这表明该过程的正确映射和层均匀化的正确实施。与以前的研究相比,非牛顿流体中各成分的应用比例使挠度有所降低。此外,使用DCPD基体的提议使得与其他材料相比能够获得低得多的挠度值,这在防弹盾牌生产领域是一项创新。