节点文献

新型有翼弹托脱壳机理研究

Research on the Discarding Characteristic of a Novel Sabot with Wing

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 于煜斌张靖王克勤

【Author】 YU Yu-bin1,ZHANG Jing1,WANG Ke-qin2(1.School of Astronautic Science and Technology,Beijing Institute of Technology,Beijing 100081,China;2.Xi’an Military Academy,Xi’an 710108,Shaanxi,China)

【机构】 北京理工大学宇航科学技术学院西安陆军学院兵种教研室

【摘要】 为了最大限度地减小脱壳弹弹托的消极质量,本文研究了一种新型有翼弹托结构,其质量比传统"马鞍形"弹托减小了1/4.文中分析了这种有翼弹托的脱壳机理,计算了其脱壳力,对该弹托的脱壳过程进行了数值仿真。最后对采用该有翼弹托的脱壳弹进行了靶场试验,结果表明,这种有翼弹托可以保证脱壳弹在炮膛内的闭气与运动稳定性,在出炮口后能够迅速、可靠地脱壳。

【Abstract】 In order to reduce the negative mass of the sabot,a novel sabot with wing configuration was designed.The mass of the novel sabot is only 3/4 of the saddle shape sabot.The discarding characteristic of the novel sabot was analyzed,the discarding force of the sabot was calculated,the discarding process of the novel sabot was simulated.Finally an experiment of the novel sabot was carried out,and the result validates that the novel sabot with wing configuration can discard rapidly and reliably.

  • 【分类号】TJ410.3
  • 【被引频次】8
  • 【下载频次】207
节点文献中: 

本文链接的文献网络图示:

本文的引文网络