首页 | 本学科首页   官方微博 | 高级检索  
     

哈尔滨四方台斜拉桥模态参数和索力识别
引用本文:侯立群,欧进萍,赵雪峰,李宏伟. 哈尔滨四方台斜拉桥模态参数和索力识别[J]. 振动与冲击, 2009, 28(5): 106-110. DOI:  
作者姓名:侯立群  欧进萍  赵雪峰  李宏伟
作者单位:1. 哈尔滨工业大学 土木工程学院,哈尔滨 150090,2. 大连理工大学 土木水利学院,大连 116024
基金项目:国家自然科学基金,国家科技支撑计划 
摘    要:桥梁的模态参数是修正有限元模型、识别损伤及桥梁状态评估的重要参数。动力测试是获得模态参数的必要途径。建立了哈尔滨四方台大桥的有限元模型;利用8个力平衡加速度传感器采用分组测试的方式测试了桥面加速度,利用压电传感器测试了斜拉索的加速度;联合NExT法和ERA法进行了斜拉桥模态参数识别,并将识别结果与有限元模型的计算结果进行了对比分析;采用拉索基频的频差拟合识别法进行频率及索力识别,并进行了实测索力与设计索力的对比分析

关 键 词:桥梁工程   动力测试   索力识别   斜拉桥   模态参数识别   
收稿时间:2008-06-13
修稿时间:2008-07-30

Identification of modal parameters and cable tension of harbin sifangtai bridge
HOU Li-qun,OU Jin-ping,ZHAO Xue-feng,LI Hong-wei. Identification of modal parameters and cable tension of harbin sifangtai bridge[J]. Journal of Vibration and Shock, 2009, 28(5): 106-110. DOI:  
Authors:HOU Li-qun  OU Jin-ping  ZHAO Xue-feng  LI Hong-wei
Affiliation:1. School of Civil and Hydraulic Engineering, Dalian University of Technology, Dalian 116024, China; 2. School of Civil Engineering, Harbin Institute of Technology, Harbin 150090, China
Abstract:Modal parameter of bridge is very important for finite element updating, damage identification and bridge condition assessment. Dynamic test is the necessary approach to obtain the modal parameter of bridge. Finite element model of Harbin Sifangtai Bridge was established, eight accelerometers with force feedback was applied to measure acceleration of bridge deck by the way of group test, piezoelectric accelerometer was applied to measure acceleration of cable, the combined method the NExT and ERA was applied to identify cable-stayed bridge modal parameter and the identification result was compared with the calculated result of finite element, frequency difference fitting method was introduced to identify frequency and tension of cable and the result was compared with the design cable tension of real bridge.
Keywords:bridge engineering  dynamic test  cable tension identification  cable-stayed bridge  modal parameters identification
本文献已被 维普 万方数据 等数据库收录!
点击此处可从《振动与冲击》浏览原始摘要信息
点击此处可从《振动与冲击》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