带缘板阻尼结构转子叶片振动特性的影响参数分析

张大义1,2,杨诚1, 夏颖1,付检伟1,洪杰1,2

振动与冲击 ›› 2019, Vol. 38 ›› Issue (10) : 221-227.

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振动与冲击 ›› 2019, Vol. 38 ›› Issue (10) : 221-227.
论文

带缘板阻尼结构转子叶片振动特性的影响参数分析

  • 张大义1,2,杨诚1, 夏颖1,付检伟1,洪杰1,2
作者信息 +

Influential parameters of rotating blades with under platform dampers

  • ZHANG Dayi1,2, YANG Cheng1, XIA Ying1, FU Jianwei1, HONG Jie1,2
Author information +
文章历史 +

摘要

针对转子叶片缘板阻尼结构设计需求,首先根据简化模型定性分析了缘板阻尼结构接触作用对刚度和阻尼带来的非线性影响;然后采用考虑正压力的分布形式和局部滑移现象的分布式摩擦力学模型,通过数值计算叶片非线性振动响应,获得了缘板阻尼结构关键参数对叶片振动特性的影响规律。研究结果表明:阻尼块质量是缘板阻尼结构设计的最关键参数,应根据最佳压紧力值确定阻尼块质量。
 

Abstract

According to the configuration design requirements of the under platform damper(UPD) in aero engines, the nonlinear stiffness and damping due to frictional contact were studied based on a simplified model of UPD.The nonlinear vibration responses of the blade with different design parameters were calculated by adopting the distributed contact model which takes account of the distributed normal load and partial slip.The influences of the design parameters of UDP on the vibration characteristics of the blade were investigated.The results indicate that the UPD mass is the pivotal parameter in the design of UPD, and it is supposed to determine it by the optimal pressing load.

关键词

叶片
/ 干摩擦 / 振动特性 / 阻尼 / 缘板阻尼结构

引用本文

导出引用
张大义1,2,杨诚1, 夏颖1,付检伟1,洪杰1,2. 带缘板阻尼结构转子叶片振动特性的影响参数分析[J]. 振动与冲击, 2019, 38(10): 221-227
ZHANG Dayi1,2, YANG Cheng1, XIA Ying1, FU Jianwei1, HONG Jie1,2. Influential parameters of rotating blades with under platform dampers[J]. Journal of Vibration and Shock, 2019, 38(10): 221-227

参考文献

[1] 陈璐璐, 马艳红, 杨鑫,等. 带干摩擦阻尼结构叶片振动响应试验[J]. 航空动力学报, 2008, 23(9):1647- 1653.
  CHEN Lulu, MA Yanhong, YANG Xin, et al. Experi-ment of vibration and response of blade with dry friction structure [J]. Journal of Aerospace Power, 2008, 23(9): 1647-1653. (in Chinese)
[2] Petrov E P, Zachariadis Z, Beretta A, et al. A study of nonlinear vibrations in a frictionally-damped turbine bladed disc with comprehensive modelling of aerody-namic effects[J]. Journal of Engineering for Gas Turbines & Power, 2012, 135(3):1239-1251.
[3] 李琳, 刘久周, 李超. 航空发动机中的干摩擦阻尼器及其设计技术研究进展[J]. 航空动力学报, 2016, 31(10):2305-2317.
  LI Lin, LIU Jiuzhou, LI Chao. Review of the dry friction dampers in aero-engine and their design technologies[J]. Journal of Aerospace Power, 2016, 31(10): 2305-2317. (in Chinese)
[4] 郝燕平, 单颖春, 朱梓根.缘板摩擦阻尼器的减振实验研究[J]. 航空动力学报, 2001, 16(1):55-58.
  HAO Yanping, SHAN Yingchun, ZHU zigen. New method to resolve vibratory response of blades with friction damper[J]. Journal of Aerospace Power, 2001, 16(1):55-58. (in Chinese)
[5] 孙莹, 刘永泉, 郝燕平,等. 带缘板摩擦阻尼片高压涡轮叶片的减振研究[J].航空发动机, 2014, 40(5):57-61.
  SUN Ying, LIU Yongquan, HAO Yanping, et al. Vibra-tion reduction of high pressure turbine blade with plat-form friction damper[J]. Aeroengine, 2014, 40(5):57-61. (in Chinese)
[6] 陈光, 洪杰, 马艳红.航空燃气涡轮发动机结构[M].北京航空航天大学出版社, 2010.
[7] Yang B D, Menq C H. Characterization of contact kin-ematics and application to the design of wedge dampers in turbomachinery blading. Part1 – Stick-slip contact kinematics[J]. Journal of Engineering for Gas Turbines & Power, 1998, 120, 410–417.
[8] Yang B D, Menq C H. Characterization of contact kin-ematics and application to the design of wedge dampers in turbomachinery blading. Part2 – Prediction of forced response and experimental verification[J]. Journal of Engineering for Gas Turbines & Power, 1998, 120, 418–423.
[9] Sanliturk K Y, Ewins D J, Stanbridge A B. Underplatform dampers for turbine blades: Theoretical modeling, analysis, and comparison with experimental data[C]// ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1999: V004T03A037-V004T03A037.
[10] 郝燕平, 朱梓根.带摩擦阻尼的叶片响应求解方法[J].航空学报, 2001, 22(5):411-414.
  HAO Yanping, ZHU zigen. New method to resolve vi-bratory response of blades with friction damper[J].Acta Aeronautica et Astronautica Sinica, 2001, 16(1):55-58. (in Chinese)
[11] 郝燕平, 朱梓根. 叶片摩擦阻尼器的优化设计方法研究[J]. 航空动力学报, 2002, 17(3):349-356.
  HAO Yanping, ZHU zigen. Optimization Design of Friction Damper of Blade[J]. Journal of Aerospace Power, 2002, 17(3):349-356. (in Chinese)
[12] Iwan W D. On a class of models for the yielding behavior of continuous and composite systems[C].  Journal of Applied Mechanics, 1967.
[13] Schwingshackl C W, Petrov E P, Ewins D J. Effects of contact interface parameters on vibration of turbine bladed disks with underplatform dampers[J]. Journal of Engineering for Gas Turbines & Power, 2011, 134(134): 032507.
[14] Sanliturk, K.Y., Ewins, D.J. Modelling two-dimensional friction contact and its application using harmonic balance method. Journal of Sound and Vibration, 1996, 193(2), 511-523.
[15] 漆文凯, 高德平. 带摩擦阻尼装置系统振动响应分析方法研究[J]. 航空动力学报, 2006, 21(1):161-167.
  QI Wenkai, GAO Deping. Study of vibration response analysis method for the dry friction damping systems [J]. Journal of Aerospace Power, 2006, 21(1):161-167. (in Chinese)
[16] Panning L, Sextro W, Popp K. Spatial dynamics of tuned and mistuned bladed disks with cylindrical and wedge-shaped friction dampers[J]. International Journal of Rotating Machinery, 2003, 9(3):219-228.
[17] Petrov E P. Explicit finite element models of friction dampers in forced response analysis of bladed disks[J]. Journal of Engineering for Gas Turbines & Power, 2007, 130(2):277-285.
[18] 郝燕平, 朱梓根. 摩擦阻尼器参数对叶片振动响应的影响[J]. 航空发动机, 2007, 33(2):18-21.
    HAO Yanping, ZHU Zigen. Effects of Friction Damper Parameters on Blade Vibration Respons[J]. Aeroengine, 2007, 130(2):277-285. (in Chinese)
[19] 吴向宇, 韩绪军, 张海洋,等. 高压涡轮工作叶片缘板阻尼结构设计分析[J]. 航空动力学报, 2014, 29(6): 1376-1381.
  WU Xiangyu, HAN Xujun, ZHANG Haiyang, et al. Analysis and design of platform damper construction for high pressure turbine blade[J]. Journal of Aerospace Power, 2014, 29(6):1376-1381. (in Chinese)
[20] 李琳, 刘久周, 李超. 干摩擦阻尼器对宽频多阶次激励减振效果分析[J]. 航空动力学报, 2016, 31(9): 2171-2180.
  LI Lin, LIU Jiuzhou, LI Chao. Analysis on damping effect of dry friction damper under wideband mul-ti-harmonic excitation.[J]. Journal of Aerospace Power, 2016, 31(9):2171-2180. (in Chinese)
[21] Zhang D, Fu J, Zhang Q, et al. An effective numerical method for calculating nonlinear dynamics of structures with dry friction: application to predict the vibration re-sponse of blades with underplatform dampers[J]. Non-linear Dynamics, 2016:1-15.
[22] Yang B D, Chu M L, Menq C H. Stick–slip–separation analysis and non-linear stiffness and damping charac-terization of friction contacts having variable normal load[J]. Journal of Sound and Vibration, 1998, 210(4): 461-481.
[23] Petrov E P, Ewins D J. Effects of damping and varying contact area at blade-disk joints in forced response analysis of bladed disk assemblies[J]. Journal of Turbomachinery, 2006, 128(2): 403-410.

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