Volume 28 Issue 10
Oct.  2013
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YU Xue-ran, LU Shan. Integrative design method of blisk considering structure strength and resonant vibration avoidance[J]. Journal of Aerospace Power, 2013, 28(10): 2235-2239.
Citation: YU Xue-ran, LU Shan. Integrative design method of blisk considering structure strength and resonant vibration avoidance[J]. Journal of Aerospace Power, 2013, 28(10): 2235-2239.

Integrative design method of blisk considering structure strength and resonant vibration avoidance

  • Received Date: 2012-10-15
  • Publish Date: 2013-10-28
  • The parametric model of blisk was established based on the software of ANSYS.The blisk model with minimum mass and sufficient structure strength,along with stress criterion of the strength design for disk,was accomplished through optimization module of ANSYS.The vibration characteristics of blisk was analyzed,and the influence of the adjustment of disk parameters and blade profile parameters on the nature frequency of blisk were studied.On this basis,the structure design method of blisk considering avoidance of low order excitation was studied through the adjustment of different structural parameters,such as rim thickness,blade lean and blade profile thickness.According to the research statistics,the adjustment of disk parameters can increase the margin between the frequencies of low order coupled vibration and 4E excitation by 2.2% at the maximum rotation speed for the drum-constrained blisk,and the margin increase can be 8% by adjustment of blade profile parameters.The integration design method of blisk considering structure strength and resonant vibration avoidance is feasible,as the margin between the frequencies of 4E excitation and 1st vibration of the final blisk with the minimum mass is up to 10.8% with insulation from 5E excitation at the loss of 4.77% mass increase.

     

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  • [1]
    黄春峰.航空发动机整体叶盘结构及发展趋势[J].现代零部件,2005(4):96-101. HUANG Chunfeng.Structure and development of blisk[J].Modern Component,2005(4):96-101.(in Chinese)
    [2]
    Chan Y J,Ewins D J.Prediction of vibration response levels of mistuned integral bladed disks(blisks):robustness studies[J].Journal of Turbomachinery,2012,134(4):044501.1-044501.7.
    [3]
    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. WANG Jianjun,XU Jiandong,LI Qihan.Analytical models of mistuned bladed disk assembles:a review[J].Turbine Technology,2004,46(4):256-259.(in Chinese)
    [4]
    葛长闯,王建军,刘永泉.失谐多级整体叶盘振动模态特性定量评价方法研究[J].航空发动机,2012,38(1):25-28. GE Changchuang,WANG Jianjun,LIU Yongquan.Quantitative assessment method of vibration mode characteristics for mistuned multistage blisk[J].Aeroengine,2012,38(1):25-28.(in Chinese)
    [5]
    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):011013.1-011013.9.
    [6]
    Zhou B,Thouverez F,Lenoir D.An adaptive control strategy based on passive piezoelectric shunt techniques applied to mistuned bladed disk [C]//Proceeding of Fifth International Conference on Advanced Computational Methods in Engineering.Liège,Belgium:University of Liège,2011:1-12.
    [7]
    WANG Mei,LU Shan,GU Yuanxing.The methods of frequency modulation of fan blade [C]//Proceeding of the 4th ICMEM.Suzhou:International Conference on Mechanical Engineering and Mechanics,2011:228-231.
    [8]
    陆山,陶冶,鲁冯杰.轮盘结构方案设计及重量预估 [C]//中国航空学会第十五届发动机结构强度与振动学术交流会论文集.杭州:中国航空学会,2010:372-379.
    [9]
    陆山,鲁冯杰.基于ANSYS的整体叶盘结构优化设计[J].航空动力学报,2012,27(6):128-1224. LU Shan,LU Fengjie.Optimization design method of blisk based on the ANASYS[J].Journal of Aerospace Power,2012,27(6):128-1224.(in Chinese)
    [10]
    吕文林.航空涡喷、涡扇发动机结构设计准则:第2册[R].北京:中国航空工业总公司发动机系统工程局,1997:269-270.
    [11]
    王延荣,田爱梅.叶/盘结构振动分析中几个问题的探讨[J].推进技术,2002,23(3):233-236. WANG Yanrong,TIAN Aimei.Several issues in the implementation of vibration analysis of bladed disk[J].Journal of Propulsion Technology,2002,23(3):233-236.(in Chinese)
    [12]
    周传月,邹经湘,闻学友,等.燃气轮机叶片-轮盘耦合振动特性计算[J].航空学报,2000,21(6):545-547. ZHOU Chuanyue,ZOU Jingxiang,WEN Xueyou,et al.Calculation of the blade-disc coupled vibration characteristics of a gas turbine[J].Acta Aeronautica et Astronautica Sinica,2000,21(6):545-547.(in Chinese)
    [13]
    赵卫强,刘永贤,鲁墨武.某航空发动机压气机叶片轮盘耦合振动分析[J].机械设计与制造,2010(5):116-118. ZHAO Weiqiang,LIU Yongxian,LU Mowu.Coupling vibration analysis of an aeroengine compressor blade-disc system[J].Machinery Design & Manufacture,2010(5):116-118.(in Chinese)
    [14]
    吕文林.航空发动机强度计算[M].北京:国防工业出版社,1988.
    [15]
    张晓东,吴虎,黄健,等.跨音速轴流压气机叶片造型及数值仿真[J].计算机仿真,2008,25(12):58-61. ZHANG Xiaodong,WU Hu,HUANG Jian,et al.Blade form and numerical investigation of transonic compressor[J].Computer Simulation,2008,25(12):58-61.(in Chinese)
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