期刊文献+

炮口阻拦装置设计与脱壳过程数值模拟

Research on Design of Muzzle Blocking Device and NumericalSimulation of Sabot Discarding Process
下载PDF
导出
摘要 为了实现弹托与弹丸在炮口处的快速分离,设计了一种平衡炮炮口阻拦装置,该装置采用了剪切螺栓和阻拦环的方式,有效避免弹托冲击对阻拦装置和炮管造成的损坏。应用该装置进行了320 mm平衡炮低速加载试验,并利用Autodyn软件对脱壳过程进行数值模拟研究。数值模拟与试验结果的对比分析,验证了数值模拟的准确性。探讨了该炮口阻拦装置用于弹托分离试验的可行性,采用该软件模拟了不同初始速度下炮口阻拦装置的工作性能。结果表明:当速度为100~150 m/s时,弹托分离效果较好;该炮口阻拦装置设计合理,弹托分离效果理想;可根据初速设计合理的阻拦装置,为相关研究提供理论参考。 To make the sabot quickly separate from the projectile in the muzzle,a kind of Davis gun muzzle blocking device was designed to block the cartridge.The way of shearing bolt and blocking ring was adopted to avoid the damage to the blocking device and barrel caused by impact.The device was applied to the low-speed loading test of 320 mm Davis gun,and the numerical simulation of the shell removal process was carried out by Autodyn software.By comparing the simulation results with the test results,the accuracy of the numerical simulation was verified,and the feasibility of the muzzle blocking device used in the separation test of projectile bracket was discussed.The working performance of muzzle blocking device at different initial velocities was simulated by the software.When the speed is about 100-150 m/s,the separation effect is better.The design of muzzle blocking device is reasonable,and the separation effect of projectile bracket is ideal.Reasonable muzzle blocking device can be designed according to the initial velocity,which can provide theoretical support for the development of related research.
作者 杨凯 江坤 YANG Kai;JIANG Kun(School of Energy and Power Engineering,Nanjing University of Science and Technology,Nanjing 210094,China)
出处 《弹道学报》 CSCD 北大核心 2021年第4期34-39,共6页 Journal of Ballistics
关键词 平衡炮 炮口阻拦装置 机械式脱壳 Davis gun muzzle blocking device sabot discarding
  • 相关文献

参考文献9

二级参考文献34

  • 1龚自正,杨继运,代福,董洪建,童靖宇,向树红,庞贺伟.CAST空间碎片超高速撞击试验研究进展[J].航天器环境工程,2009,26(4):301-306. 被引量:15
  • 2王金贵.超高速碰撞的弹托分离技术[J].高压物理学报,1993,7(2):143-147. 被引量:9
  • 3管公顺,张伟,庞宝君,哈跃.铝球弹丸高速正撞击薄铝板穿孔研究[J].高压物理学报,2005,19(2):132-138. 被引量:19
  • 4柳森,李毅,黄洁,罗锦阳,谢爱民,石安华.用于验证数值仿真的Whipple屏超高速撞击试验结果[J].宇航学报,2005,26(4):505-508. 被引量:28
  • 5STILP A J, HOHLER Y. High velocity impact dynamics [M]. New York:John Wiley & Sons, Inc, 1990.
  • 6LESAGE F, RAW M J. Navier-Stokes computation of the aerodynamics of symmetric sabot separation[C]. 13th International Symposium on Ballistics. Stockholm, Sweden: IBC, 1992.
  • 7YEAN K L, CHANG H T. High-resolution navier-stokes computations of a sabot separating from a gun-launched projectile with turbulence model[C]. 14th International Symposium on Ballistics. Quebec, Canada: IBC, 1993.
  • 8CHAMPIGNY P, ESPINEY P, CERONI D. Computation of sabot discard using chimera technique[C]. 17th International Symposium on Ballistics. Midrand, South Africa: IBC, 1998.
  • 9MIKHAIL A, HEAVY K. Sabot opening lift force: analysis, CFD, and test[C]. 38th AIAA Aerospace Sciences Meeting & Exhibit. Reno, Nevada, USA: AIAA, 2000.
  • 10王金贵.超高速碰撞的弹托分离技术[R].绵阳:中物院流体物理研究所,1991.

共引文献202

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部