| Citation: | SUN Chao, QI Wenkai, NIU Nanke. Analysis of vibration reduction characteristics and test methods of blisk damping ring[J]. Journal of Aerospace Power, 2025, 40（5）：20230569 doi: 10.13224/j.cnki.jasp.20230569
|
A real compressor blisk was taken as the research object, and the damping ring vibration reduction characteristics were analyzed for three node diameter modes of the blisk. A finite element model of the blisk was established. Based on the global-local unified sliding model, a vibration response analysis method suitable for annular damper system was developed, and the vibration response of a blisk under harmonic excitation was simulated using this method. A test system was designed to excite the pitch diameter vibration of the blisk. The rationality of the finite element model and the effectiveness of the calculation method were verified by tests. The results showed that the damping ring had a good effect on the vibration reduction of various modes, up to 60%. The test results agreed well with the simulation results, and the natural frequency errors were within 5%. The research results have some reference value to the vibration reduction design of the integral bladed disc structure in engineering.
| [1] |
王红建,贺尔铭. 叶片失谐对叶盘结构振动特性的影响[J]. 西北工业大学学报,2009,27(5): 645-650. WANG Hongjian,HE Erming. Exploring key features of blade mistuning effects on vibration characteristics of bladed disks[J]. Journal of Northwestern Polytechnical University,2009,27(5): 645-650. (in Chinese
WANG Hongjian, HE Erming. Exploring key features of blade mistuning effects on vibration characteristics of bladed disks[J]. Journal of Northwestern Polytechnical University, 2009, 27(5): 645-650. (in Chinese)
|
| [2] |
GRIFFIN J H,HOOSAC T M. Model development and statistical investigation of turbine blade mistuning[J]. Journal of Vibration and Acoustics,1984,106(2): 204-210. doi: 10.1115/1.3269170
|
| [3] |
IRRETIER H. Coupled vibrations of blades in bending-bending-torsion and disks in out-of-plane and in-plane motion[R]. St. Louis, Mo,US:American Society of Mechanical Engineers,Design Engineering Technical Conference,1979.
|
| [4] |
叶先磊,王建军,朱梓根,等. 大小叶盘结构连续参数模型和振动模态[J]. 航空动力学报,2005,20(1): 66-72. YE Xianlei,WANG Jianjun,ZHU Zigen,et al. Continuous parameter model and vibration modal of splitter vane rotor[J]. Journal of Aerospace Power,2005,20(1): 66-72. (in Chinese
YE Xianlei, WANG Jianjun, ZHU Zigen, et al. Continuous parameter model and vibration modal of splitter vane rotor[J]. Journal of Aerospace Power, 2005, 20(1): 66-72. (in Chinese)
|
| [5] |
陈玉刚. 整体叶盘振动特性分析与硬涂层阻尼减振设计研究[D]. 大连: 大连理工大学,2017. CHEN Yugang. Analysis of vibration characteristics of integral bladed disk and study on damping and vibration reduction design of hard coating[D]. Dalian: Dalian University of Technology,2017. (in Chinese
CHEN Yugang. Analysis of vibration characteristics of integral bladed disk and study on damping and vibration reduction design of hard coating[D]. Dalian: Dalian University of Technology, 2017. (in Chinese)
|
| [6] |
HASSAN M. Vibration analysis of turbomachinery blades[D]. Hartford,Connecticut,US: Faculty of Rensselaer Polytechnic Institute,2008.
|
| [7] |
王进. 行波激励作用下涂层整体叶盘振动特性测试与分析[D]. 沈阳: 东北大学,2020. WANG Jin. Measurement and analysis of vibration characteristics of coated blisk under traveling wave excitation[D]. Shenyang: Northeastern University,2020. (in Chinese
WANG Jin. Measurement and analysis of vibration characteristics of coated blisk under traveling wave excitation[D]. Shenyang: Northeastern University, 2020. (in Chinese)
|
| [8] |
漆文凯. 涡轮转子叶片叶根阻尼装置减振特性分析及试验研究[D]. 南京: 南京航空航天大学,2005. QI Wenkai. Analysis and experimental study on vibration reduction characteristics of turbine rotor blade root damping device[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2005. (in Chinese
QI Wenkai. Analysis and experimental study on vibration reduction characteristics of turbine rotor blade root damping device[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2005. (in Chinese)
|
| [9] |
漆文凯,高德平. 摩擦阻尼减振设计中的局部滑动问题[J]. 航空学报,2006,27(5): 805-809. QI Wenkai,GAO Deping. Microslip study on friction damping and its application in design of vibration reduction[J]. Acta Aeronautica et Astronautica Sinica,2006,27(5): 805-809. (in Chinese
QI Wenkai, GAO Deping. Microslip study on friction damping and its application in design of vibration reduction[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(5): 805-809. (in Chinese)
|
| [10] |
朱永新. 带冠叶片摩擦减振特性研究[D]. 南京: 南京航空航天大学,2007. ZHU Yongxin. Study on friction vibration reduction characteristics of shrouded blades[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2007. (in Chinese
ZHU Yongxin. Study on friction vibration reduction characteristics of shrouded blades[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2007. (in Chinese)
|
| [11] |
吴绵绵. 涡轮叶片摩擦阻尼减振设计方法研究[D]. 南京: 南京航空航天大学,2010. WU Mianmian. Study on design method of friction damping vibration reduction of turbine blades[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2010. (in Chinese
WU Mianmian. Study on design method of friction damping vibration reduction of turbine blades[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2010. (in Chinese)
|
| [12] |
陈俊杰. 带冠叶盘干摩擦阻尼减振特性研究[D]. 南京: 南京航空航天大学,2015. CHEN Junjie. Study on vibration reduction characteristics of dry friction damping of bladed disk with crown[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2015. (in Chinese
CHEN Junjie. Study on vibration reduction characteristics of dry friction damping of bladed disk with crown[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015. (in Chinese)
|
| [13] |
温伟,漆文凯. 基于整体叶盘环形摩擦阻尼器减振分析及设计[J]. 航空动力学报,2020,35(4): 777-782. WEN Wei,QI Wenkai. Vibration reduction analysis and design of friction ring damper in blisk[J]. Journal of Aerospace Power,2020,35(4): 777-782. (in Chinese
WEN Wei, QI Wenkai. Vibration reduction analysis and design of friction ring damper in blisk[J]. Journal of Aerospace Power, 2020, 35(4): 777-782. (in Chinese)
|
| [14] |
牛南轲,漆文凯,许正华. 管式减涡器阻尼结构减振特性及设计方法[J]. 航空动力学报,2024,39(6): 20220469. NIU Nanke,QI Wenkai,XU Zhenghua. Damping characteristics and design method of tubular vortex reducer damper[J]. Journal of Aerospace Power,2024,39(6): 20220469. (in Chinese
NIU Nanke, QI Wenkai, XU Zhenghua. Damping characteristics and design method of tubular vortex reducer damper[J]. Journal of Aerospace Power, 2024, 39(6): 20220469. (in Chinese)
|
| [15] |
徐自力,谷伟伟,吕强,等. 基于微动滑移模型的叶片阻尼结构参数研究[J]. 西安交通大学学报,2007,41(5): 507-511. XU Zili,GU Weiwei,LYU Qiang,et al. Study on damping structure parameters of blades based on the microslip model[J]. Journal of Xi’an Jiaotong University,2007,41(5): 507-511. (in Chinese
XU Zili, GU Weiwei, LYU Qiang, et al. Study on damping structure parameters of blades based on the microslip model[J]. Journal of Xi’an Jiaotong University, 2007, 41(5): 507-511. (in Chinese)
|
| [16] |
谷伟伟,徐自力,胡哺松,等. 微滑移阻尼叶片最优正压力的影响因素分析[J]. 西安交通大学学报,2008,42(7): 828-832. GU Weiwei,XU Zili,HU Busong,et al. Influence of structural parameters on optimal normal load of microslip damped blades[J]. Journal of Xi’an Jiaotong University,2008,42(7): 828-832. (in Chinese
GU Weiwei, XU Zili, HU Busong, et al. Influence of structural parameters on optimal normal load of microslip damped blades[J]. Journal of Xi’an Jiaotong University, 2008, 42(7): 828-832. (in Chinese)
|
| [17] |
LAXALDE D,THOUVEREZ F,LOMBARD J P. Forced response analysis of integrally bladed disks with friction ring dampers[J]. Journal of Vibration and Acoustics,2010,132(1): 011013. doi: 10.1115/1.4000763
|
| [18] |
ZUCCA S,DI MAIO D,EWINS D J. Measuring the performance of underplatform dampers for turbine blades by rotating laser Doppler vibrometer[J]. Mechanical Systems and Signal Processing,2012,32: 269-281. doi: 10.1016/j.ymssp.2012.05.011
|
DownLoad:
