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聚能射孔弹的正交试验方法 总被引:1,自引:1,他引:0
在聚能射孔弹的研究中应用正交试验方法,以确定聚能射孔弹各结构因素对性能的影响及主要因素的交互作用对性能的影响.选择药型罩锥角、药型罩壁厚、装药结构、壳体厚4个对射孔弹穿深有主要影响的参数,用L8(27)正交试验表设计了4因素2水平的正交试验方案.分析试验数据得出了各因素及交互作用对射孔弹性能的影响程度,罩锥角(A)对射孔弹穿深的影响最大,为首要因素;罩壁厚(B)及装药结构(C)对射孔弹穿深的影响很大,为次要因素;A×B交互作用对射孔弹穿深的影响较大,大于壳体厚(D)的影响;得出了A1B2C2D2为最优方案,并得到了试验验证. 相似文献
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讨论了炸高达到100射孔弹直径(CD)时射孔弹的穿透性能,到目前为止该炸高远远超过了应用的标准范围(2~7CD).在实验过程中确定了射孔弹在钢靶中的穿透深度,并研究出一种计算法来描述该结果.实验过程中获得的数据大幅度提高了工程计算法在射孔弹穿透深度建模中的应用能力.这是首次在炸高很大时使用计算方法来估算穿透深度,与实验结果取得了很好的一致性. 相似文献
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本文主要从射孔弹穿靶最基本的原理入手,对不同靶板材料对射孔弹穿深的影响进行初步分析和研究,引入国外较为成熟的常用不同靶板材料的穿深性能转换的经验公式,提出一种基础的同等条件下射孔弹性能的评价方法。 相似文献
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A theoretical analysis on detonation wave propagation in a double-layer shaped charge (DLSC) is performed. Numerical simulations using the AUTODYN software are carried out to compare the distinctions between jet formations in DLSC and ordinary shaped charge (OSC), in particular, the OSC made using a higher detonation velocity explosive, which is treated as the outer layer charge in the DLSC. The results show that the improved detonation velocity ratio and radial charge percentage of outer-to-inner layer charge are conducive to the formation of a convergent detonation wave, which contributes to enhancement of jet tip velocity in DLSC. The thickness and mass percentages of liner flowing into jet in DLSC closely follow the exponential distribution along the radial direction, but the percentages in DLSC and the mass of effective jet, which have significant influence on the penetration depth, are lower than those in OSC with the outer layer charge. This implies that the total charge energy is the major factor controlling the effective jet formation, which is confirmed by the verification tests using flash X-ray system and following penetration tests. The numerical simulation and test results compare well, while penetration test results indicate that the performance of DLSC is not better than that of OSC with the outer layer charge, due to the differences in jet formation. 相似文献
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采用数值模拟对比了3 1/2 in*型等孔径射孔弹与同规格常规深穿透射孔弹在井筒内装枪极限情况下的射流形态,并采用地面模拟试验对比了两者孔眼一致性.数值模拟结果表明,后者药型罩在压垮过程中形成了细长的锥形射流,尾部形成了粗大的杵体,而前者能够形成一段高速的杆式射流,不易受炸高的影响;地面模拟装枪侵彻钢靶结果表明,前者射孔后在套管上形成的平均孔径为12.3 mm,孔径稳定性为96.7%,比后者平均孔径提高了2.3 mm,孔径稳定性提高了20.4%,说明其具有较大的孔径和好的孔眼一致性,同时也验证了数值模拟结果与实验值相符.3 1/2 in型等孔径射孔弹地面模拟装枪侵彻混凝土靶平均穿深为810 mm,表明其具有深穿透特点. 相似文献
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以渤海油田稠油油藏的胶结疏松地质条件为研究背景,有针对性地设计了一种新型7in高孔密大破片射孔弹。采用AOTUDY和ANSYS/LS-DYNA软件对射孔弹的壳体爆炸破片和射流形成进行数值仿真分析,进行地面模拟装枪穿钢靶试验和单发射孔弹破片收集试验。数值仿真的破片形成效果和射流形态与地面试验结果吻合较好。新型射孔弹的大破片尺寸大于9.53mm,占有率达到85.95%,明显优于常规射孔弹的破片率。在渤海油田实际应用中,壳体形成大破片效果良好,多数留在枪体内,保证了射孔作业安全和后续完井工艺的顺利开展。 相似文献
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The effective jet length between the virtual origin (VO) point and the target surface is very important for the calculation of a shaped charge jet penetration. A numerical approach to determine the exact position of the VO of a small caliber shaped charge jet is presented in this paper. The numerical approach includes shaped charge jet formation algorithm using explicit Autodyn solver and estimates the precise location of the VO point using the hydrocode analysis. This is particularly important when the experimental flash X-ray radiograph is not available. The proposed VO model approach was validated by firing four small caliber shaped charges against concrete targets. The maximum difference between the experimental penetration depth and that calculated using the presented VO approach was less than 4%. 相似文献
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为满足复杂地质条件下射孔作业的需要,选择25 g装药量的BH38RDX-46-89型射孔弹进行性能优化.运用微差法设计药型罩与装药结构,用数值模拟分析射流成型和侵彻,按设计配方进行打靶实验.优化后的89型大孔径射孔弹BH38RDX-46-89性能有显著提升,其穿钢靶孔径达到了16 mm,穿深提高到了111 mm,达到了大孔径深穿透的效果.实际应用表明该结构可以推广应用,该设计思路与采用的理论分析、结构设计仿真及试验相结合的优化设计方法对进一步研发系列大孔径深穿透射孔弹有着一定的指导参考意义. 相似文献