摘要:
为系统评估非致命动能弹丸(Non-Lethal Kinetic Projectiles,NLKP)对人体胸部的冲击安全性,本文设计并制备了一种结构可调、兼容仿真实验的一体化三肋胸部物理模型。首先通过弹体发射平台,在 29 m/s 与 61 m/s 速度下对 SIR-X 弹丸模型进行刚性壁动力学验证,获得的力–时间曲线与北约《联合工程出版物第 99 号》(NATO Allied Engineering Publication-99,AEP-99)标准走廊吻合良好,证明了弹丸模型的可靠性。进一步使用该弹丸进行 56 m/s 和 86.5 m/s 速度下的胸部冲击实验,测得胸壁位移及黏性准则(Viscous Criterion,VC)的最大值 VCmax 均落入 AEP-99 标准验证走廊范围内,表明该模型在中低速冲击(≤ 90 m/s)条件下具有良好的动态响应一致性与预测精度。仿真与实验最大误差分别为 16% 和 21%。弹丸硬度增加(Soft 到 Hard)在 56 m/s 与 86.5 m/s 工况下使 VCmax 分别由 0.298 升至 0.336、由 0.765 升至 0.856,高能工况放大效应更显著。肋间距变化(0.8S₀–1.2S₀)对峰值位移和接触力影响约 ±6%,VCmax 波动 5.7%–6.2%,整体处于工程可接受范围。与 SHTIM 对比,本文模型在 56/86.5 m/s 下的位移–时间响应更贴合走廊中线(VCmax=0.308/0.803,均在推荐区间),SHTIM 在高能工况略低于下限,验证了本模型在响应精度与伤害判据一致性上的优势。针对 NS、CONDOR、SIR-X 和 RB1FS 四种典型弹丸,在 60–90 m/s 速度范围内开展系统仿真,揭示了不同弹丸结构和材料对胸部损伤风险的影响机制。高速冲击(100–120 m/s)下,模型软组织层主导能量吸收与耗散,肋骨层峰值应力随速度显著升高并超过屈服极限,存在严重骨折风险。厚度敏感性分析显示,软组织层厚度对吸能和变形的调控作用最为突出。研究结果为 NLKP 冲击伤害评估及防护装备优化提供了重要理论与技术支撑。
Abstract:
To systematically evaluate the thoracic safety of non-lethal kinetic projectiles (NLKP), a structurally adjustable and simulation-compatible three-rib physical chest model was designed and fabricated. The projectile representation was first validated through rigid-wall impacts at 29 m/s and 61 m/s on a controllable gas-launch platform. The measured force–time histories agreed well with the AEP-99 corridors, confirming the fidelity of the projectile model. Further chest-impact experiments were then conducted using the validated projectile model at 56 m/s and 86.5 m/s. The measured chest-wall displacements, together with the maximum value of the viscous criterion (VCmax), all fell within the validation corridors specified in the NATO Allied Engineering Publication-99 (AEP-99), demonstrating that the proposed model exhibits excellent dynamic-response consistency and predictive accuracy under medium- and low-velocity impacts at or below 90 m/s. The largest deviations between simulation and experiment were 16% and 21%, respectively. A projectile-hardness scan (Soft/Medium/Hard) showed that VCmax increased from 0.298 to 0.336 at 56 m/s and from 0.765 to 0.856 at 86.5 m/s, indicating a more pronounced risk amplification at higher energies. For rib-spacing levels of 0.8S₀/S₀/1.2S₀, peak displacement/force changed by about ±6% and VCmax shifted by 5.7%–6.2%, remaining within an engineering-acceptable band. Compared with the Surrogate Human Thorax for Impact Model (SHTIM), the proposed model adhered more closely to the corridor mid-line at 56/86.5 m/s and yielded VCmax values of 0.308/0.803 (both within the recommended ranges), whereas SHTIM slightly underestimated the high-energy case, confirming an advantage in response fidelity and criterion consistency. Based on the validated setup, systematic finite-element analyses were performed for four representative NLKP—NS, CONDOR, SIR-X, and RB1FS—over 60–90 m/s to elucidate how projectile structure and material govern injury risk. Additional high-velocity simulations (100–120 m/s) showed that the soft-tissue layer dominated energy absorption and dissipation, whereas the rib layer experienced rapidly increasing peak von Mises stress that exceeded the yield limit, revealing a severe fracture risk at elevated speeds. A thickness-sensitivity study demonstrated that the soft-tissue-layer thickness exerted the strongest regulation on total absorbed energy and deformation, while the rib-layer thickness was most effective for limiting peak deflection; the skin-layer thickness had only minor influence within the tested range. These results establish an integrated experiment–simulation framework for thoracic impact evaluation of NLKP, quantify velocity-dependent and layer-specific injury mechanisms, and identify key structural parameters—especially soft-tissue thickness—that control energy management and deformation, providing support for injury assessment and for optimizing protective equipment and testing protocols.