摘要
本文分析了直升机载雷达振动、冲击环境条件特点,探讨了直升机载雷达总体结构环境适应性设计思路,提出了直升机载雷达隔振缓冲设计方法、隔振缓冲措施以及实验验证结果。
The vibration and impact environment condition of helicopter-borne radar are analyzed;the design conception of helicopter-borne radar system structure environmental adaptability is discussed;the method and measures for helicopter-borne radar vibration isolation and buffer are presented,and the experimental verification result is given.
出处
《火控雷达技术》
2010年第4期9-13,共5页
Fire Control Radar Technology
关键词
隔振缓冲
振源频率
动刚度
vibration isolation and buffer
vibration source frequency
kinematical rigidity
