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火箭仪器舱仪器安装板的振动控制试验研究
Experimental study on vibration control for instrument board of apparatus cabin of launch vehicle
【摘要】 本文在对长 甲运载火箭仪器舱进行了试验模态分析的基础上 ,对长 甲运载火箭仪器舱进行了可控约束阻尼层主被动一体化振动控制试验研究 ,研究结果表明 ,可控约束阻尼层结构对火箭仪器舱这一大型复杂结构进行振动控制是非常有效的
【Abstract】 The experimental modal analysis of the apparatus cabin of CZ 3a launch vehicle is performed firstly.In response of the dynamic characteristics of the apparatus cabin the hybrid vibration control for instrument board of apparatus cabin is experimentally performed by applying controllable constrained layer damping.Research results show it is very effective that applying the controllable constrained layer damping suppresses the vibration of the apparatus cabin of the launch vehicle.
【关键词】 火箭;
振动控制;
可控约束阻尼层;
【Key words】 Rocket; Vibration controls; Controllable constrained layer damping;
【Key words】 Rocket; Vibration controls; Controllable constrained layer damping;
- 【文献出处】 宇航学报 ,Journal of Astronautics , 编辑部邮箱 ,2002年01期
- 【分类号】V421.31
- 【被引频次】9
- 【下载频次】207