为实现同心发射筒上的系留盖体在燃气作用下打开，讨论盖体分为4片被燃气吹开和盖体整体被燃气吹开2种方案，并对盖体被燃气吹开过程进行模拟分析。计算结果表明，盖体分为4块被燃气吹开速度快，筒内压强降低速度快。因此，盖体分为4块的方案对筒内导弹发射环境更有利。
In order to realize the automatic opening of the reserved cover on concentric canister launcher under the action of exhaust gas, two schemes are discussed: the reserved cover is divided into 4 pieces first and then opened by the exhaust gas and the reserved cover as a whole is opened by the exhaust gas.The opening process of the reserved cover in above two cases is simulated by numerical method.The calculation results show that the reserved cover was opened faster and the pressure inside the concentric canister launcher decreased faster when the reserved cover was divided into 4 pieces.therefore, it is more beneficial for missile launching when the reserved cover is divided into 4 pieces.
2021,43(1): 176-179 收稿日期：2019-10-14
DOI：10.3404/j.issn.1672-7649.2021.01.033
分类号：TH123
作者简介：吴利民(1977-),男,高级工程师,主要从事导弹发射装置研究与设计工作
参考文献：
[1] 边金尧, 徐松林, 钱海鹰. 同心发射筒研究现状[J]. 舰船科学技术, 2012, 34(11): 1-5
[2] 韩煜宇, 吴利民. 燃气流公共排导和同心筒技术在舰载导弹垂直发射装置中的应用分析[J]. 舰船科学技术, 2007, 29(S1): 1-5
[3] YAGLA J J. Concentric canister launcher[J]. Naval Engineers Journal, 1997, 109: 313-330
[4] MOORHEAD S B. The latest ship weapon launchers-The vertical launching system[J]. Naval Engineers Journal, 1981(4): 152-167
[5] 苗佩云, 袁曾凤. 同心发射筒燃气开盖技术[J]. 北京理工大学学报, 2004, 4(24): 283-285
[6] 翟建龙. 同心发射筒内燃气流对密封盖冲击的数值仿真[J]. 科技情报开发与经济, 2006, 16(19): 150-151
[7] 孙建中. 美国海军的新型舰载垂直发射装置[J]. 现代防御技术, 2001, 29: 34-37
[8] 王福军. 计算流体动力学分析-CFD软件原理与应用[M]. 北京: 清华大学出版社, 2004.
