Effects of dry friction damping on forced vibration response of mistuned bladed disk

被引：1
|
作者：
Liu Y. [1 ]
Shangguan B. [2 ]
Xu Z. [3 ]
机构：
[1] School of Environmental and Municipal Engineering, Xi'an University of Architecture and Technology, Xi'an
[2] Xi'an Thermal Power Research Institute Co., Ltd., Xi'an
[3] State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi'an Jiaotong University, Xi'an
来源：
Xu, Zili | 2016年 / Xi'an Jiaotong University卷 / 50期
关键词：
Antialiasing hybrid frequency-time domain method; Dry friction damping; Mistuned blade disc; Three-dimensional friction contact;
D O I：
10.7652/xjtuxb201602019
中图分类号：
学科分类号：
摘要：
In the existing vibration characteristics research of mistuned bladed disk system with nonlinear dry friction damping structures, we have to encounter establishment of nonlinear friction contact model and solution of high degree of freedom nonlinear systems. Here the anti-aliasing hybrid frequency-time domain method and three-dimensional microslip friction contact model are chosen to evaluate the forced vibration response of a mistuned bladed disk with dry friction damping structure. The friction damping effect on forced vibration response of mistuned bladed disk, and the vibration characteristics of mistuned bladed disk under the condition of friction mistuned are investigated. It is found that the nonlinear friction vibration damping structure enables to inhibit vibration of mistuned bladed disk system with a 9.53% average amplitude decrease. The friction damping effect on each blade is different, and the corresponding optimal initial normal load of each blade reaching the optimal damping effect is not identical too. The normal contact stiffness mistuning and initial normal load mistuning also have the damping effect on the mistuned bladed disk. When the mistuned strength and mistuned distribution of the normal contact stiffness mistuning are the same as those of mistuned bladed disk, the friction damping effect attenuates in comparison with the situation of friction tuned, and the average decline of vibration amplitude reduces by 3.45%. © 2016, Editorial Office of Journal of Xi'an Jiaotong University. All right reserved.
引用
收藏
页码：111 / 117
页数：6
相关论文
共 13 条
  • [1] Bai B., Bai G., Tong X., Et al., Research on vibration problem of integral mistuned bladed disk assemblies at home and abroad, Journal of Aerospace Power, 29, 1, pp. 91-103, (2014)
  • [2] Lin C.C., Mignolet M.P., An adaptive perturbation scheme for the analysis of mistuned bladed disks, ASME Journal of Engineering for Gas Turbines and Power, 119, pp. 153-160, (1997)
  • [3] Griffin J.H., Sinha A., The interaction between mistuning and friction in the forced response of bladed disk assemblies, ASME Journal of Engineering for Gas Turbines and Power, 107, pp. 205-211, (1985)
  • [4] Petrov E.P., A method for forced response analysis of mistuned bladed disks with aerodynamic effects included, ASME Journal of Engineering for Gas Turbines and Power, 132, 6, (2010)
  • [5] Cha D., Sinha A., Statistics of response of a mistuned and frictionally damped bladed disk assembly subjected to white noise and narrow band excitations, Probabilistic Engineering Mechanics, 21, pp. 384-396, (2006)
  • [6] Petrov E.P., Ewins D.J., Advanced modeling of under platform friction dampers for analysis of bladed disk vibration, ASME Journal of Turbomachinery, 129, pp. 143-150, (2007)
  • [7] Petrov E.P., Ewins D.J., Method for analysis of nonlinear multi harmonic vibrations of mistuned bladed disks with scatter of contact interface characteristics, ASME Journal of Turbomachinary, 127, pp. 128-136, (2005)
  • [8] Jareland M.H., Csaba G., Friction damper mistuning of a bladed disk and optimization with respect to work, ASME Turbo Expo 2000: Power for Sea, and Air, (2000)
  • [9] Wang H., He E., Yu S., Forced response characteristics of bladed disks with disordered dry friction, Journal of Aerospace Power, 21, 4, pp. 711-715, (2006)
  • [10] Wang A., Long Q., Forced response characteristics of bladed disks with random mistuned non-linear friction damping, Journal of Aerospace Power, 26, 1, pp. 178-184, (2011)
12