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叶盘结构盘片耦合振动特性的参数敏感性 被引量:5

Parametric sensitivity for coupling vibration characteristics of bladed disk
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摘要 在参数化建模、求解的基础上重点研究了叶盘结构盘片耦合振动频率转向特性、由结构参数随机失谐引起的振动局部化特性对结构设计参数变化的敏感性.对盘片耦合振动频率转向特性的研究发现,随着轮盘扇区间耦合刚度或叶片刚度的变化,频率转向间隙曲线的改变具有碗状形式;对振动局部化特性的研究表明,以轮盘扇区间耦合刚度和结构参数失谐强度为自变量的失谐响应放大因子曲面呈类马鞍形;响应放大阈值现象存在与否,与轮盘扇区间耦合刚度的大小直接相关.若选择位于鞍部的轮盘扇区间耦合刚度-失谐强度组合参数设计,失谐响应放大因子最多能够被减小37.5%. Based on parametric modeling and solution of bladed disk, the parametric sensitivity for coupling vibration characteristics of bladed disk were studied, of which the frequency veering and modal localization caused by random mistuning of structure parameters were mainly focused on. The study on coupling vibration characteristics of frequency veering of bladed disk uncovers that the loci of the gap of frequency veering is a bowl-style-curve while the inter-sector stiffness or bladed stiffness varies within a certain range. And the study on localization vibration characteristics finds that there exists a quasi-saddle-surface while the amplification factor is related to inter-sector stiffness and mistuning strength. The latter reveals that the existence of threshold of amplification factor against mistuning strength depends on the strength of inter-sector stiffness. It is also found that a proper choice of inter-sector stiffness and mistuning strength in saddle could lead to a suppression of amplification factor of 37.5 %.
作者 王培屹 李琳
出处 《航空动力学报》 EI CAS CSCD 北大核心 2014年第1期81-90,共10页 Journal of Aerospace Power
关键词 参数敏感性 失谐 频率转向 模态局部化 响应放大 碗状结构 类马鞍面 蒙特卡洛模拟 parametric sensitivity mistuning frequency veering modal localization response amplification bowl-style-structure quasi-saddle-surface Mote Carlo simulation
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  • 1王建军,于长波,李其汉.错频叶盘结构振动模态局部化特性分析[J].航空动力学报,2009,24(4):788-792. 被引量:13
  • 2王建军,许建东,李其汉.失谐叶片-轮盘结构振动局部化的分析模型[J].汽轮机技术,2004,46(4):256-259. 被引量:12
  • 3叶先磊,王建军,朱梓根,李其汉.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. 被引量:7
  • 4Castanier M P, Pierre C. Modeling and analysis of mistuned bladed disk: status and emerging directions[J]. Journal of Propulsion and Power,2006,22(2) :384-396.
  • 5Wei S T, Pierre C. Statistical analysis of the forced response of mistuned cyclic assemblies[J]. AIAA Journal, 1990,28(5) : 861-868.
  • 6Choi B K, Lentz J, Rivas Guerra A J, et al. Optimization of intentional mistuning patterns for the reduction of the forced response effects of unintentional mistuning [J]. Journal of Engineering for Gas Turbines and Power,2003, 125(1) :131-140.
  • 7Castanier M P, Ottarsson G, Pierre C. A reduced order modeling technique for mistuned bladed disks[J]. Journal of Vibration and Acoustics,1997,119(3):439-447.
  • 8Castanier M P, Pierre C. Investigation of the combined effects of intentional and random mistuning on the forced response of bladed disks[R]. AIAA-98-3720,1998.
  • 9Castanier M P, Pierre C. Using intentional mistuning in the design of turbomachinery rotors[J]. AIAA Journal, 2002, 40(10) :2077-2086.
  • 10Ottarsson G,Pierre C. On the effects of interblade coupling on the statistics of maximum forced response amplitudes in mistuned bladed disks [C]//Proceedings of the 36th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. New Orleans, LA, United States: AIAA. 1995,3070-3078.

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