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兵工学报 ›› 2015, Vol. 36 ›› Issue (1): 1-11.doi: 10.3969/j.issn.1000-1093.2015.01.001

• 论文 •    下一篇

发射装药发射安全性评定方法研究

芮筱亭1, 冯宾宾1,2, 王燕1, 黎超1, 陈涛3   

  1. (1.南京理工大学 发射动力学研究所, 江苏 南京 210094; 2.中国兵器工业标准化研究所, 北京 100089;
  • 收稿日期:2014-04-23 修回日期:2014-04-23 上线日期:2015-03-14
  • 作者简介:芮筱亭(1956—),男,教授,博士生导师
  • 基金资助:
    国防科技工业局基础产品创新科研专项(2012年);高等学校博士学科点专项科研项目(20113219110025);国家自然科学 基金项目(11102089)

Research on Evaluation Method for Launch Safety of Propellant Charge

RUI Xiao-ting1, FENG Bin-bin1,2, WANG Yan1, LI Chao1, CHEN Tao3   

  1. (1.Institute of Launch Dynamics, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China;2.China Ordnance Industrial Standardization Research Institute, Beijing 100089, China; 3.Mechanics Experiment Center, School of Science, Nanjing University of Science and Technology, Nanjing 210094, Jiangsu, China)
  • Received:2014-04-23 Revised:2014-04-23 Online:2015-03-14

摘要: 发射装药发射安全性问题严重制约现代火炮武器的发展,成为各军事强国竞相攻关解决的重大理论与技术难题。从揭示发射装药引起膛炸的机理入手,通过理论、计算、试验3个方面连续17年的系统深入研究,引入起始动态活度比新概念,建立了我国首个基于发射装药起始动态活度比的发射装药发射安全性评定方法兵器行业标准和国家军用标准。文中包括:发射装药发射安全性评定原理、发射装药发射安全性评定流程、发射装药膛内力学环境试验方法、发射装药动态挤压破碎试验方法、发射装药起始动态活度比试验方法、发射装药发射安全性判据的确定方法、发射装药发射安全性评定方法,并成功用于工程实践,为科学评估发射装药发射安全性提供了系统的理论依据、技术手段和技术标准。

关键词: 兵器科学与技术, 发射装药, 发射安全性, 评定方法, 起始动态活度比, 试验研究, 判据

Abstract: The launch safety problem of gun propellant charge has severely restricted the development of modern gun, and has already become major theoretical and technical problems which has attracted considerable attention. A new concept, namely the initial dynamic vivacity ratio of propellant charge is presented based on 17 years of profound research on theoretical analysis, computation and test which reveals the mechanism of bore premature caused by propellant charge. The industry standard and military standard of launch safety evaluation method were set up. The evaluation principle of launch safety for propellant charge, the evaluation process of launch safety for propellant charge, the mechanics environment test method of propellant charge in chamber, the test method of dynamic stress and fracture of propellant charge, the test method of initial dynamic vivacity ratio of propellant charge, the approach to determine the criterion of launch safety for propellant charge, and the evaluation method of launch safety for propellant charge are introduced. The methods have been in the engineering practice successfully. The theoretical basis, technical approaches and technical standards are provided for the scientific evaluation of launch safety of propellant charge.

Key words: ordnance science and technology, propellant charge, launch safety, evaluation method, initial dynamic vivacity ratio, test research, criterion

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