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航天器系统级减振/隔振应用研究及其进展
引用本文:陈健,冯淑红,柳征勇,唐国安.航天器系统级减振/隔振应用研究及其进展[J].强度与环境,2013(5):37-42.
作者姓名:陈健  冯淑红  柳征勇  唐国安
作者单位:[1]上海宇航系统工程研究所,上海201108 [2]复旦大学力学与工程科学系,上海200433
摘    要:研制减振、隔振系统对于改善卫星在火箭主动段飞行中的动态环境,降低卫星主结构的低频动力学载荷,提高卫星的可靠性具有重要的实际应用价值。对系统级减振、隔振在航天中应用进行了综述,并对目前国内航天在整星减振隔振研制中遇到的问题及进展情况,进行了介绍,对后续发展进行了展望。

关 键 词:减振  隔振  航天器

Development of application for planet system-level vibration reduction
CHEN Jian,FENG Shuhong,LIU Zhengyong,TANG Guoan.Development of application for planet system-level vibration reduction[J].Structure & Environment Engineering,2013(5):37-42.
Authors:CHEN Jian  FENG Shuhong  LIU Zhengyong  TANG Guoan
Institution:1 Shanghai Institute of Aerospace System Engineering, Shanghai 201108, China; 2 Department of Mechanics and Engineering Science, Fudan University Shanghai 200433, China)
Abstract:Development of vibration reduction that play the actual value for improve the dynamical environment of planet during the boost phase of launch vehicle, reduce dynamic load during low-frequency phase of main-structure of planet. Synthesize the application system-level vibration reduction exist in the aerospace area, and introduce the development about whole planet vibration reduction aboard, also preview the more research.
Keywords:vibration reduction  vibration separation  space vehicle
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