首页 | 本学科首页   官方微博 | 高级检索  
     检索      

涡轮带冠叶片干摩擦阻尼减振试验
引用本文:陈香,朱靖,李光辉,王春健.涡轮带冠叶片干摩擦阻尼减振试验[J].航空动力学报,2012,27(4):817-823.
作者姓名:陈香  朱靖  李光辉  王春健
作者单位:中国航空工业集团公司 中国燃气涡轮研究院, 四川 江油 621703
摘    要:设计一套涡轮带冠叶片干摩擦阻尼减振试验系统,并利用该试验系统对阻尼块与叶冠之间不同接触紧度、不同接触面积以及采用不同材料阻尼块时涡轮叶片动力特性和减振效果进行了分析研究.结果表明接触紧度、阻尼块的接触面积、材料以及外部激振力共同影响涡轮叶片的减振效果,共同决定该系统是否存在最优正压力以及最优正压力存在时的范围或大小.另外,激振力的变化将导致叶片的响应、系统阻尼比、共振频率以及最优正压力等一系列参数变化.试验结果能够为理论计算提供数据验证,为指导涡轮带冠叶片的减振设计提供依据. 

关 键 词:涡轮叶片    干摩擦    阻尼    最优正压力    试验
收稿时间:2011/6/22 0:00:00
修稿时间:2/9/2012 12:00:00 AM

Experiment on dry friction damping of shrouded turbine blades
CHEN Xiang,ZHU Jing,Li Guang-hui and Wang Chun-jian.Experiment on dry friction damping of shrouded turbine blades[J].Journal of Aerospace Power,2012,27(4):817-823.
Authors:CHEN Xiang  ZHU Jing  Li Guang-hui and Wang Chun-jian
Institution:China Gas Turbine Establishment, Aviation Industry Corporation of China, Jiangyou Sichuan 621703, China
Abstract:A dry friction damping test system of shrouded turbine blades was designed.The effects of different mounting tightness and contact areas between damping block, blade shroud and different materials of damping block on dynamical characteristic and damping of the turbine blades were studied with this system.The results show that damping of the turbine blades is affected by mounting tightness,contact area,materials of damping block and excitation force,which also determin whether the damping system has best vertical press,and dominates its range and domain under the existence of best vertical press.Moreover,change of the excitation force can induce the changing a series of experimental parameters,such as response of the turbine blades,damping ratio of the system,resonance frequency and best vertical press.Those results can provide the experimental verification for theoretical arithmetic and provide further insight into damping design of the shrouded turbine blades.
Keywords:turbine blade  dry friction  damping  best vertical press  experiment
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号