期刊文献+

舰用燃气轮机框架模型的模态参数识别 被引量:1

APPLICATION OF MULTIMODE DIRECT FITTING METHOD IN MODAL IDENTIFICATION OF THE BASE OF GAS TURBINE
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摘要 本文采用一种有理正交多项式──多模态曲线拟合法对一舰用燃气轮机框架模型进行了实验模态分析。以Forsythe复正交多项式作为频响函数的理论值,用实测的频响函数建立系数矩阵,来寻找使目标函数最小的最优值。本文在HP9826微机上建立了测试、数据采集及参数识别等系统识别软件。给出了具有工程实用意义的前五阶振动模态参数,识别结果和有限元计算相比较,令人满意。 In the paper, an orthogonal polynomial analysis method-Multimode Direct Fitting Method is developed. Taking the model base of a marine gas turbine as an example, the measured Transfer Functions are used to establish the coefficient matrix and the Forsythe Orthogonal Polynomial is adopted in the identification of the modal parameters of the frame. The complete analysis software of modal identification in frequency domain induding the software of data acquisition and parameter estimation has been estab fished on a HP9826 personal computer. The agreement between the identified results and that of the finite element analysis shows that the estimation is effective and satifactory. The modal parameters of first 5 orders which are of practical significance in engineering have been successfully obtained in the experiment.
出处 《振动与冲击》 EI CSCD 北大核心 1996年第3期7-11,共5页 Journal of Vibration and Shock
关键词 多模态拟合法 燃气轮机 框架 模态识别 舰艇 multi-modal fitting method, platform of gas turbines, modal identification
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参考文献4

  • 1许克勤,博士学位论文,1991年
  • 2傅志方,振动模态分析与参数辨识,1990年
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同被引文献15

  • 1崔广涛,彭新民,苑希民,陶毅,安刚.高拱坝泄洪振动水弹性模型[J].水利学报,1996,28(4):1-9. 被引量:9
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  • 3彭伟 袁景侠.模态参数的整体正交多项式识别法[J].动态分析测试技术,1988,(3):1-9.
  • 4Richardson M H, Formenti D L, Parameter estimation from frequency response measurements using the rational fraction polynomial method [A], In: D J DeMichele,Proc of 1^st International Modal Analysis Conference [ C l,Florida: Union College, 1982, 167-180.
  • 5Richardson M H, Formenti D L, Global curve fitting of frequency response measurements using the rational fraction polynomial method[A], In: D J DeMichele. Proc of 3^rd International Modal Analysis Conference[C]. Florida:Union College, 1985. 390-397.
  • 6Richardson M H. Global frequency & damping estimates form frequency response measurements using the rational fraction polynomial method [A]. In: D J DeMichele.Proc of 4^th International Modal Analysis Conference[ C].Florida: Union College, 1986. 465 -470.
  • 7Carrascoca L I, Busturia. Global Experiment modal analysis, a comparison of different methods[A]. In: D J DeMichele. Proc of 3^rd International Modal Analysis Conference[C]. Florida: Union College, 1985. 311 -317.
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  • 10张燕飞,安春利,张胜勇.复合材料柔性喷管试验模态分析[J].固体火箭技术,1997,20(4):7-11. 被引量:1

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