| 航天器仪器安装板附加约束阻尼层设计与振动抑制验证 |
| |
| 引用本文： | 张家雄,张华山,曹晓瑞,张会杰,魏小彪.航天器仪器安装板附加约束阻尼层设计与振动抑制验证[J].航天器环境工程,2016,33(5):540-544. |
| |
| 作者姓名： | 张家雄 张华山 曹晓瑞 张会杰 魏小彪 |
| |
| 作者单位： | 1. 中国运载火箭技术研究院 研究发展中心, 北京 100076;2. 北京航天材料及工艺研究所, 北京 100076;3. 湖北三江航天洪峰控制有限公司, 孝感 432000 |
| |
| 基金项目： | 国防基础科研计划基金项目（编号：JCKY2013601B） |
| |
| 摘 要： | 针对某航天器仪器安装板在噪声载荷作用下振动响应过大的情况,提出采取附加约束阻尼层的振动抑制措施。文章首先介绍约束阻尼层的应用情况,简要说明了约束阻尼层减振的原理;随后以航天器典型仪器安装板为研究对象,通过对比同等噪声载荷下约束阻尼层附加前、后仪器安装板上的振动响应,分析了振动抑制情况。结果显示,仪器安装板附加约束阻尼层后,仪器设备安装处随机振动均方根加速度平均降低1.56 d B(16.4%)。
|
| 关 键 词： | 飞行器 仪器安装板 约束阻尼层 振动抑制 |
| 收稿时间： | 2016/4/19 0:00:00 |
| 修稿时间： | 2016/9/13 0:00:00 |
Constrained damping layer design and vibration suppression verification for vehicle instrument installation board |
| |
| ZHANG Jiaxiong,ZHANG Huashan,CAO Xiaorui,ZHANG Huijie,WEI Xiaobiao.Constrained damping layer design and vibration suppression verification for vehicle instrument installation board[J].Spacecraft Environment Engineering,2016,33(5):540-544. |
| |
| Authors: | ZHANG Jiaxiong ZHANG Huashan CAO Xiaorui ZHANG Huijie WEI Xiaobiao |
| |
| Institution: | 1. R & D Center, China Academy of Launch Vehicle Technology, Beijing 100076, China;2. Aerospace Research Institute of Materials & Processing, Beijing 100076, China;3. Hubei Sanjiang Hongfeng Control Equipment Co. Ltd., Xiaogan 43200, China |
| |
| Abstract: | To solve the problem of the vibration response overrun of a space vehicle''s instrument installation board excited by the acoustic load, a vibration suppression method of adding a constrained damping layer is put forward. First, the application and the principle of the vibration reduction of the constrained damping layer are discussed. Then with the typical instrument installation board of the vehicle as the research object, the vibration reduction is analyzed by comparing the vibration response before and after adding the constrained damping layer with the same acoustic excitation. The results show that reduction of the RMS acceleration response in the place of the instrument installation is nearly 1.56dB(16.4%) after the constrained damping layer is added to the instrument installation board. |
| |
| Keywords: | space vehicle instrument installation board constrained damping layer vibration suppression |
| 本文献已被 CNKI 等数据库收录！ |
| 点击此处可从《航天器环境工程》浏览原始摘要信息 |
| 点击此处可从《航天器环境工程》下载免费的PDF全文 |
|
