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