Page 77 - 《爆炸与冲击》2023年第2期
P. 77

第 43 卷    第 2 期                   爆    炸    与    冲    击                       Vol. 43, No. 2
                2023 年 2 月                    EXPLOSION AND SHOCK WAVES                          Feb., 2023

               DOI:10.11883/bzycj-2022-0202


                 波形控制器对杀伤战斗部破片飞散特性影响研究                                                                 *


                                               刘    伟,梁争峰,阮喜军,屈可朋

                                            (西安近代化学研究所,陕西 西安 710065)

                  摘要: 为提升杀伤战斗部破片轴向飞散的集中度,提高战斗部的轴向杀伤威力,提出使用波形控制器控制破片的
               飞散方向。基于爆轰波在波形控制器界面发生反射的规律以及                      Shapiro  公式,设计了波形控制器的形状,使用         LS-DYNA
               有限元软件和     ALE(arbitrary Lagrange-Euler)算法对破片的飞散过程进行数值计算,结合战斗部原理样机静爆试验,验
               证了使用波形控制器改善破片飞散特性方法的合理性。对比了有无波形控制器时破片飞散过程的差异,对无波形控
               制器以及波形控制器材料分别为尼龙、聚氨酯和聚四氟乙烯(polytetrafluoroethylene,PTFE)时杀伤战斗部的破片飞散速
               度和破片飞散角规律进行了分析。结果表明:波形控制器可以减小战斗部中心和两端位置的破片飞散速度大小差异,
               使中心到两端位置的破片飞散方向角变化均匀,破片在轴向的分布更加均匀;不同材料的波形控制器对破片飞散特性
               影响不同,波形控制器的使用减小了破片飞散角,增大了破片分布密度,提升了破片飞散的集中度。破片飞散角数值
               计算值与试验计算值误差在          6.53%  之内,与无波形控制器的杀伤战斗部原理样机相比,含波形控制器且材料为尼龙、
               聚氨酯和   PTFE  的战斗部原理样机破片飞散角分别减小了              40.00%、 44.00%  和  46.67%。
                  关键词: 杀伤战斗部;波形控制器;Shapiro         公式;破片飞散特性;破片飞散速度;破片飞散角
                  中图分类号: O389   国标学科代码: 13035   文献标志码: A

                       A study on the influence of wave shape controller on fragment
                              scattering characteristics of fragmentation warhead


                                      LIU Wei, LIANG Zhengfeng, RUAN Xijun, QU Kepeng
                               (Xi’an Modern Chemistry Research Institute, Xi’an 710065, Shaanxi, China)

               Abstract:  In order to improve the uniformity of the fragments of the fragmentation warhead and enhance the axial lethality of
               the warhead, it was proposed to use a wave shape controller to control the scattering direction of the fragments. The shape of
               the wave shape controller was designed based on the law of detonation wave reflection at the wave shape controller interface
               and the Shapiro formula. The LS-DYNA software and ALE(arbitrary Lagrange-Euler) algorithm were used to numerically
               simulate the scattering process of fragments, and the static explosion test of the warhead prototype was carried out to verify the
               rationality  of  using  the  wave  shape  controller  to  improve  the  scattering  characteristic  of  fragments.  The  difference  in  the
               fragment  scattering  processes  with  and  without  the  wave  shape  controller  were  compared.  The  law  of  fragment  scattering
               velocity and scattering angle of the warhead was analyzed and summarized when there was no wave shape controller and when
               the wave shape controller materials were nylon, polyurethane and PTFE(polytetrafluoroethylene), respectively. The results
               show that the wave shape controller can reduce the difference in the scattering velocities of the fragments between the center
               and both ends of the warhead, and evenly change the direction angles of the fragments scattering from the center to both ends,
               so that the fragments are distributed more uniformly along the axial direction. The wave shape controllers made of different
               materials have different effects on the scattering characteristics of the fragments, while the use of the wave shape controller




                 *  收稿日期: 2022-05-11;修回日期: 2022-07-21
                   基金项目: 国防重大基础研究专项(05020501)
                   第一作者: 刘 伟(1992- ),男,硕士研究生,1091205427@qq.com
                   通信作者: 梁争峰(1972- ),男,博士,研究员,2042lzf@sohu.com


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