期刊文献+

面向型号设计的直升机生存力评价方法初探

Preliminary Study of Helicopter Survivability for Engineering Design
在线阅读 下载PDF
导出
摘要 为满足直升机型号设计中的生存力设计要求,提出了适应直升机工程应用的生存力设计评估方法,该方法以直升机在战场中被敌方雷达发现的概率、被敌方武器击中的概率以及被杀伤概率为基础,建立直升机的生存力评估计算模型。然后以国外两型直升机为算例,通过对比分析加装防护前后的生存力数值,验证了方法的可行性,也为未来直升机生存力设计提出了建议。 For meeting the requirement of helicopter survivability design,the paper presented the method of evaluating the survivability by releasing fixed wing aircraft,and it included the probability of the helicopter was found by the enemy's radar in the battlefield,the probability of its being hit by the enemy's weapon,and the probability of being killed.Taking two helicopters for example,the paper analyzed their numerical probability of survivability before and after adding protective device, and the results showed feasibility of the method was developed,in addition,some suggestion had proposed for helicopter survivability design.
作者 徐明 李黔 XU Ming;LI Qian(China Helicopter Research and Development Institute,Jingdezhen 333001,China)
出处 《直升机技术》 2018年第4期12-15,共4页 Helicopter Technique
关键词 直升机 生存力 雷达 武器 helicopter survivability radar weapon
  • 相关文献

参考文献2

二级参考文献19

  • 1裴扬,宋笔锋,韩庆.基于有限元模型的飞机几何描述算法研究[J].西北工业大学学报,2004,22(5):567-571. 被引量:9
  • 2裴扬 宋笔锋 李占科.一种基于DMECA的飞机致命性部件辩识软件[J].机械科学与技术,2004,23:109-112.
  • 3MIL-HDBK-336-2,Survivability aircraft nonnuclear airframe[S].Washington DC:Dept of Defense,1983.
  • 4GJB/Z202-2001,飞机非核生存力通用指南[S].北京:国防科工委军标出版发行部出版,2002.
  • 5MIL-HDBK-336-1,Survivability aircraft nonnuclear general criteria[S].Washington DC:Dept of Defense,1988.
  • 6Ball R E.The fundamentals of aircraft combat survivability analysis and design[M].2nd ed.Reston:AIAA,2003.
  • 7宋笔锋 韩庆.飞机易损性指标计算的基本理论与方法(Ⅰ)[J].现代防御技术,1999,27(4):38-45.
  • 8Kiwan A R.An overview of High-Explosive (HE) blast damage mechanisms and vulnerability prediction methods[R].ARL-TR-1468,1997.
  • 9魏惠之,朱鹤松.米-24D武装直升机等效靶研究[R].GF85786,1992.
  • 10朱鹤松,高世泽.武装直升机易损性分析[R].GF85783,1992.

共引文献15

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