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军用直升机振动与噪声控制技术
引用本文:刘孝辉,徐新喜,白松,杨猛,王伟.军用直升机振动与噪声控制技术[J].直升机技术,2013(1):67-72.
作者姓名:刘孝辉  徐新喜  白松  杨猛  王伟
作者单位:军事医学科学院卫生装备研究所,天津,300161
摘    要:介绍了军用直升机振动与噪声的来源、传播途径及危害,重点论述了当前国内外军用直升机振动与噪声控制技术的原理及应用情况,对未来军用直升机振动与噪声控制技术的发展前景进行了展望。

关 键 词:军用直升机  振动控制技术  噪声控制技术

Vibration and Noise Control Technology on Military Helicopters
Authors:LIU Xiaohui  XU Xinxi  BAI Song  YANG Meng  WANG Wei
Institution:(Institute of Medical Equipment, Academy of Military Medical Sciences, Tianjin 300161, China)
Abstract:The causes and transmission routes as well as the effect of the vibration and noise on mil-itary helicopters were introduced in this paper. The principle and application of the current vibrationand noise control technology on domestic and overseas military helicopters were mainly dealt with. Meanwhile, the future development prospect of the vibration and noise control technology on militaryhelicopters was looked forward.
Keywords:military helicopters  vibration control technology  noise control technology
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