留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

碰摩作用下盘片榫连结构接触特性的响应分析

马辉 王迪 太兴宇 能海强 闻邦椿

马辉, 王迪, 太兴宇, 能海强, 闻邦椿. 碰摩作用下盘片榫连结构接触特性的响应分析[J]. 航空动力学报, 2015, 30(9): 2203-2211. doi: 10.13224/j.cnki.jasp.2015.09.020
引用本文: 马辉, 王迪, 太兴宇, 能海强, 闻邦椿. 碰摩作用下盘片榫连结构接触特性的响应分析[J]. 航空动力学报, 2015, 30(9): 2203-2211. doi: 10.13224/j.cnki.jasp.2015.09.020
MA Hui, WANG Di, TAI Xing-yu, NAI Hai-qiang, WEN Bang-chun. Contact characteristics response analysis of blade-disc dovetail structure under rubbing condition[J]. Journal of Aerospace Power, 2015, 30(9): 2203-2211. doi: 10.13224/j.cnki.jasp.2015.09.020
Citation: MA Hui, WANG Di, TAI Xing-yu, NAI Hai-qiang, WEN Bang-chun. Contact characteristics response analysis of blade-disc dovetail structure under rubbing condition[J]. Journal of Aerospace Power, 2015, 30(9): 2203-2211. doi: 10.13224/j.cnki.jasp.2015.09.020

碰摩作用下盘片榫连结构接触特性的响应分析

doi: 10.13224/j.cnki.jasp.2015.09.020
基金项目: 

教育部新世纪人才支持计划(NCET-11-0078)

中央高校基本科研业务费专项资金(N130403006)

详细信息
    作者简介:

    马辉(1978-),男,河北安平人,副教授,博士,主要从事转子动力学、非线性振动、旋转机械故障诊断研究.

  • 中图分类号: V231.92

Contact characteristics response analysis of blade-disc dovetail structure under rubbing condition

  • 摘要: 以某压气机燕尾形榫连结构为研究对象,基于ANSYS有限元软件,建立了盘片的有限元模型.用脉冲力模拟局部碰摩时的碰摩力,分析了两种碰摩情况对榫连结构接触特性的影响,首先分析了侵入量为定值时,不同转速对榫连结构接触特性的影响,接着分析了当转速为定值时,不同侵入量对榫连结构接触特性的影响.研究结果表明:随着转速的升高,榫连结构的最大接触压力和最大接触滑移距离不断的增加,最大接触压力变化规律变得更加复杂,而最大接触滑移距离变化规律逐渐趋于稳定并且最大接触滑移距离之间的变化幅度减小.随着侵入量的增加,榫连结构的最大接触压力以及最大接触滑移距离都会增大,但过大的侵入量将导致最大接触滑移距离发生突变.通过分析不同工况下几个节点接触压力及接触滑移距离的频谱响应,发现碰摩会产生转频的高倍频成分,当转频的倍频成分接近叶片固有频率时会出现倍频幅值放大现象.

     

  • [1] 魏大盛,王延荣.榫连结构的高应力梯度及破坏分析[J].北京航空航天大学学报,2010,36(10):1184-1188. WEI Dasheng,WANG Yanrong.On the high stress gradient and failure analysis of dovetail attachments[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(10):1184-1188.(in Chinese)
    [2] 林香,黄致建,郝艳华.弧形燕尾型榫连接组件三维接触分析[J].武汉理工大学学报:信息与管理工程版,2010,32(3):427-429. LIN Xiang,HUANG Zhijian,HAO Yanhua.Three dimensional contact analysis of arc-dovetail components[J].Journal of Wuhan University of Technology:Information and Management Engineering,2010,32(3):427-429.(in Chinese)
    [3] Sinclair G B,Cormier N G,Griffin J H,et al.Contact stresses in dovetail attachments finite element modeling[J].Journal of Engineering for Gas Turbines and Power,2002,124(1):182-189.
    [4] Sinclair G B,Cormier N G.Contact stresses in dovetail attachments:physical modeling[J].Journal of Engineering for Gas Turbines and Power,2002,124(2):325-331.
    [5] Sinclair G B,Cormier N G.Contact stresses in dovetail attachments alleviation via precision crowning[J].Journal of Engineering for Gas Turbines and Power,2003,125(4):1033-1041.
    [6] Padova C,Barton J,Dunn M G,et al.Experimental results from controlled blade tip-shroud rubs at engine speed[J].Journal of Turbomachinery,2007,129(4):713-723.
    [7] Lesaffre N,Sinou J J,Thouverez F.Contact analysis of a flexible bladed-rotor[J].European Journal of Mechanics A:Solids,2007,26(3):541-557.
    [8] 马辉,太兴宇,李焕军,等.旋转叶片-机匣碰摩模型及试验研究综述[J].航空动力学报,2013,28(9):2055-2069. MA Hui,TAI Xingyu,LI Huanjun,et al.Literature survey of rub-impact model and experiment of rotating blade and casing[J].Journal of Aerospace Power,2013,28(9):2055-2069.(in Chinese)
    [9] Legrand M,Batilly A,Magnain B,et al.Full three-dimensional investigation of structural contact interactions in turbomachines[J].Journal of Sound and Vibration,2012,331(11):2578-2601.
    [10] Legrand M,Batilly A, Pierre C.Numerical investigation of abradable coating removal in aircraft engines through plastic constitutive law[J].Journal of Computational and Nonlinear Dynamics,2012,7(1):011010.1-011010.11.
    [11] 刘书国,洪杰,陈萌.航空发动机叶片-机匣碰摩过程的数值模拟[J].航空动力学报,2011,26(6):1282-1288. LIU Shuguo,HONG Jie,CHEN Meng.Numerical simulation of the dynamic process of aeroengine blade-to-case rub-impact[J].Journal of Aerospace Power,2011,26(6):1282-1288.(in Chinese)
    [12] Sinha S K.Non-linear dynamic response of a rotating radial Timoshenko beam with periodic pulse loading at the free-end[J].International Journal of Nonlinear Mechanics,2005,40(1):113-149.
    [13] 太兴宇,马辉,谭祯,等.脉冲力加载下的叶片-机匣动力学特性研究[J].东北大学学报:自然科学版,2012,33(12):1758-1761. TAI Xingyu,MA Hui,TAN Zhen,et al.Research on dynamic characteristics of blade-casing with impulse loading[J].Journal of Northeastern University:Natural Science,2012,33(12):1758-1761.(in Chinese)
    [14] Turner K,Adams M.Simulation of engine blade tip-rub induced vibration[R].ASME Paper GT2005-68217,2005.
    [15] Turner K,Dunn M,Padova C.Airfoil deflection characteristics during rub evenrs[J].Journal of Turbomachinery,2012,134(1):011018.1-011018.7.
    [16] Kou H J,Yuan H Q.Rub-inducednon-linear vibrations of arotating large deflection plate[J].International Journal of Non-Linear Mechanics,2014,58:283-294.
    [17] 洪杰,刘书国,张大义,等.小型短寿命涡扇发动机涡轮叶片疲劳失效分析[J].航空动力学报,2012,27(3):604-609. HONG Jie,LIU Shuguo,ZHANG Dayi,et al.Fatigue failure analysis of turbine blade in miniature shor-life turbofan engine[J].Journal of Aerospace Power,2012,27(3):604-609.(in Chinese)
    [18] Barton J,Dunn M G,Manwarong S,et al.Development of an experimental capability to produce controlled blade tip-shroud rubs at engine speed[J].Journal of Turbomachinery,2005,127(4):726-735.
    [19] Anthony G.Parameter study of blade disk/casing interactions through direct contact in aeroengine assemblies[D].Montréal,Canada:McGill University,2008.
    [20] Jiang J.Investigation of friction in blade/casing rub and its effect on dynamics of a rotor with rub[M].Aachen:Shaker Verlag,2001.
  • 加载中
计量
  • 文章访问数:  1096
  • HTML浏览量:  153
  • PDF量:  558
  • 被引次数: 0
出版历程
  • 收稿日期:  2014-03-11
  • 刊出日期:  2015-09-28

目录

    /

    返回文章
    返回