期刊文献+

叶片随机失谐与叶盘结构共振特性分析 被引量:6

Investigating Further Resonant Response Characteristics of Disk with Randomly Mistuned Blades
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摘要 叶片随机失谐对叶盘动力特性具有重要影响,导致叶盘系统模态局部化和受迫响应的急剧增大。文章针对叶片随机失谐,利用Monte Carlo分析方法,研究失谐叶盘结构模态局部化特性以及不同系统频率下的共振响应特性。随机失谐分布采用质量失谐和刚度失谐两种形式,着重分析其对叶片占优系统模态族的局部化程度、相应失谐共振响应及其最大振幅放大因子的影响规律。研究结果表明,失谐对叶盘低阶弯曲模态族的局部化程度影响最大,对应的最大振幅放大因子也相应较大。 Aim.The second paragraph of the introduction of the full paper points out what we believe to be the shortcomings of Refs.2 through 5;so,we propose investigating further.Sections 1,2 and 3 explain the results of our investigation.The core of section 2 is that we use the Monte Carlo method to study the mode localization characteristics of a disk with randomly mistuned blades under the condtions of mass mistuning and stiffness mistuning respectively,focusing on the blade-dominated mode.The core of section 3 consists of:(1) we investigate statistically the resonant response characteristics of a disk with randomly mistuned blades under the conditions of mass mistuning and stiffness mistuning respectively;(2) we study the influence of blade mistuning on the resonant response of the disk with the maximum amplitude magnification factor.The simulation results,given in Figs.3 through 12,and their analysis show preliminarily that blade mistuning has the greatest influence on the low-order flexible mode localization,thus increasing the maximum amplitude magnification factors of blades.
出处 《西北工业大学学报》 EI CAS CSCD 北大核心 2011年第2期189-193,共5页 Journal of Northwestern Polytechnical University
基金 国家自然科学基金(50775181)资助
关键词 叶盘结构 随机失谐 共振特性 MONTE Carlo 振幅放大因子 resonance turbomachine blades Monte Carlo methods disk randomly mistuned blade resonant response maximum amplitude magnification factor
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参考文献9

  • 1Sinha, Chen S. Probabilistic Analysis of Forced Response of a Bladed Disk Assembly with Various Mistuning Distributions . 1988, AIAA-1988-2399.
  • 2Srinivasan A V. Flutter and Resonant Vibration Characteristics of Engine Blades. ASME Journal of Engineering for Gas Turbines and Power, 1997, 119:742 -775.
  • 3Castanier M P, Ottarsson G. A Reduced-Order Modeling Technique for Mistuned Bladed Disks. Journal of Vibration and Acous- tics. 1997, 119:439 -447.
  • 4Castanier M P, Pierre C. Investigation of the Combined Effects of Intentional and Random Mistuning on the Forced Response of Bladed Disks. AIAA-98-3720.
  • 5Rivas-Guerra A J, Mignolet M P. Maximum Amplification of Blade Response Due to Mistuning: Localization and Modes Shapes Aspects of the Worst Disks. ASME Paper GT-2002-30323, ASME Turbo Expo 2002, Amsterdam, the Netherlands.
  • 6Kenyon J A, Griffin J H, Feiner D M. Maximum Bladed Disk Forced Response from Distortion of a Structural Mode. Journal of Turbomachinery, 2003, 125 (2) :352 - 363.
  • 7Choi B K, Lentz J, et al. Optimization of Intentional Mistuning Patterns for the Reduction of the Forced Response Effects of Un- intentional Mistuning: Formulation and Assessment. Journal of Engineering for Gas Turbines and Power. 2003, 125:131 - 140.
  • 8Yu Changbo, Wang Jianjun, Li Qihan. on the Individual and Combined Effects of Intentional Mistuning Coupling and Damping on the Forced Response of Bladed Disks. Proceedings of ASME Turbo Expo 2008 : Power for Land, Sea and Air, 2008, 9 - 12.
  • 9王红建,贺尔铭,赵志彬.频率转向特征对失谐叶盘模态局部化的作用[J].中国机械工程,2009,10(1):82-85. 被引量:19

二级参考文献11

  • 1Afolabi D, Mehmed O. On Curve Veering and Flutter of Rotating Blades[J]. ASME Journal of Engineering for Gas Turbines and Power, 1994, 116:702-708.
  • 2Bladh R, Pierre C, Castanier M P, et al. Dynamic Response Predictions for a Mistuned Industrial Turbomachinery Rotor Using Reduced--order Modeling[J]. Journal of Engineering for Gas Turbines and Power, 2002, 124:311-324.
  • 3Kenyon J A, Griffin J H, Feiner D M. Maximum Bladed Disk Forced Response from Distortion of a Structural Model[J]. ASME Journal of Turbomachinery, 2003, 125:352-363.
  • 4Ewins D J, Imregun M. Vibration Modes of Packeted Bladed Disks[J]. ASME Journal of Vibration, Acoustics, Stress and Reliability in Design, 1984, 106:175- 180.
  • 5Wei S T, Pierre C. Localization Phenomena in Mistuned Assemblies with Cyclic Symmetry Part 2 : Forced Vibrations[J]. ASME Journal of Vibration, Acousties, Stress and Reliability in Design, 1988, 110:439-449.
  • 6Ottarsson G, Pierre C. A Transfer Matrix Approach to Free Vibration Localization in MistunedBladed Assemblies[J]. Journal of Sound and Vibration, 1996, 197 (5): 589-618.
  • 7Rivas--Gueera A Jr Mignolet M P. Maximum Ampli fication of Blade Response due to Mistuning: Localiza tion and Mode Shape Aspects of the Worst Disks[J] Journal of Turbomachinery, 2003, 125:442-454.
  • 8Kenyon J A, Griffin J H, Kim N E. Frequency Veering Effects on Mistuned Bladed Disk Forced Response [C]//39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Huntsville, Alabama: AIAA, 2003-497G.
  • 9Castanier M P, Ottarsson G. A Reduced--order Modeling Technique for Mistuned Bladed Disks[J]. Journal of Vibration and Acoustics, 1997, 119:439-447.
  • 10Kenyon J A, Griffin J H, Kim N E. Sensitivity of Turned Bladed Disk Response to Frequency Veering [J]. Journal of Engineering for Gas Turbines and Power, 2005, 127:835-842.

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