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旋转叶片-柔性机匣碰摩振动响应分析
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  • 英文篇名:Rub vibration responses of rotating blade and flexible casing
  • 作者:郭旭民 ; 孙祺 ; 马辉 ; 孙帆
  • 英文作者:GUO Xumin;SUN Qi;MA Hui;SUN Fan;School of Mechanical Engineering and Automation, Northeastern University;Key Lab of Vibration and Control of Aero-Propulsion Systems Ministry of Education of China, Northeastern University;State Key Lab of Mechanical System and Vibration, Shanghai Jiao Tong University;
  • 关键词:圆柱壳 ; 叶片-柔性机匣碰摩 ; 振动响应 ; 节径振动
  • 英文关键词:cylindrical shell;;blade-flexible casing rubbing;;vibration response;;pitch diameter vibration
  • 中文刊名:ZDCJ
  • 英文刊名:Journal of Vibration and Shock
  • 机构:东北大学机械工程与自动化学院;东北大学航空动力装备振动及控制教育部重点实验室;上海交通大学机械系统与振动国家重点实验室;
  • 出版日期:2019-03-15
  • 出版单位:振动与冲击
  • 年:2019
  • 期:v.38;No.337
  • 基金:国家自然科学基金(11772089);; 中央高校基金科研业务费专项资金(N170308028);; 辽宁省高等学校创新人才支持计划(LR2017035);; 机械系统与振动国家重点实验室课题资助项目(MSV201707)
  • 语种:中文;
  • 页:ZDCJ201905024
  • 页数:7
  • CN:05
  • ISSN:31-1316/TU
  • 分类号:170-176
摘要
以旋转叶片-柔性机匣为研究对象,基于ANSYS分析软件,考虑叶片旋转导致的离心刚化,旋转软化和科氏力效应,分别采用悬臂梁和圆柱壳来模拟叶片和柔性机匣,分析了碰摩导致的机匣及叶片振动,并与将机匣简化为集中质量点模型进行了对比。研究结果表明,考虑机匣柔性时能观察到由碰摩诱发的机匣节径振动,并且碰摩力和叶片振动响应相对于集中质量点模型均呈现出降低趋势。
        A rotating blade and a flexible casing were taken as the study object, and influences of centrifugal stiffening, spin softening and Coriolis force caused by blade-rotating were considered. A cantilever beam and a cylindrical shell were used to imitate the blade and flexible casing, respectively and analyze their vibrations due to their rubbing based on the software ANSYS. The simulation results were compared with those obtained during the casing being simplified as a lumped mass point. The results showed that the pitch diameter vibration of the casing induced by rubbing is observed when considering the casing's flexibility; rubbing force and blade vibration response have a declining trend compared with those obtained using the casing's lumped mass point model.
引文
[1] SINHA S K. Dynamic characteristics of a flexible bladed-rotor with Coulomb damping due to tip-rub[J]. Journal of Sound and Vibration, 2004, 273: 875-919.
    [2] LESAFFRE N, SINOU J J, THOUVEREZ F. Stability analysis of rotating beams rubbing on an elastic circular structure[J]. Journal of Sound and Vibration, 2007, 299(1): 1005-1032.
    [3] 太兴宇,马辉,谭祯,等. 叶片-机匣系统碰摩振动响应分析[J]. 振动、测试与诊断, 2014, 34(2): 280-287. TAI Xingyu, MA Hui, TAN Zhen, et al. Analysis of vibration response during blade-casing rub events[J]. Journal of Vibration, Measurement & Diagnosis, 2014, 34(2): 280-287.
    [4] MA H, TAI X, HAN Q, et al. A revised model for rubbing between rotating blade and elastic casing[J]. Journal of Sound and Vibration, 2015, 337: 301-320.
    [5] HEMMATNEZHAD M, RAHIMI G H, TAJIK M, et al. Experimental, numerical and analytical investigation of free vibrational behavior of GFRP-stiffened composite cylindrical shells[J]. Composite Structures, 2015, 120: 509-518.
    [6] RODRIGUES L, SILVA F M A, GON?ALVES P B, et al. Effects of modal coupling on the dynamics of parametrically and directly excited cylindrical shells[J]. Thin-Walled Structures, 2014, 81: 210-224.
    [7] SONG X, ZHAI J, CHEN Y, et al. Traveling wave analysis of rotating cross-ply laminated cylindrical shells with arbitrary boundaries conditions via Rayleigh-Ritz method[J]. Composite Structures, 2015, 133: 1101-1115.
    [8] 王宇,罗忠. 薄壁圆柱壳构件受迫振动的响应特征研究[J]. 振动与冲击, 2015, 34(7): 103-108. WANG Yu, LUO Zhong. Forced vibration response characteristics of thin cylindrical shell[J]. Journal of Vibration and Shock, 2015, 34(7): 103-108.
    [9] 李晖,孙伟,张永峰,等. 约束态薄壁圆柱壳固有频率的精确测试[J]. 东北大学报(自然科学版),2013, 34(9): 1314-1318. LI Hui, SUN Wei, ZHANG Yongfeng, et al. Accurate test of natural frequency of constrained thin cylindrical shell[J]. Journal of Northeastern University (Natural Science), 2013, 34(9): 1314-1318.
    [10] 曹志远. 板壳振动理论[M]. 北京:中国铁道出版社,1989.
    [11] CHEN G. Study on the recognition of aero-engine blade-casing rubbing fault based on the casing vibration acceleration[J]. Measurement, 2015, 65: 71-80.
    [12] CHEN G. Simulation of casing vibration resulting from blade-casing rubbing and its verifications[J]. Journal of Sound and Vibration, 2016, 361: 190-209.
    [13] TURNER K, ADAMS M, DUNN M. Simulation of engine blade tip-rub induced vibration[C]//Proceedings of GT2005, Ren-Tahoe. Nevada, 2005.
    [14] TURNER K, DUNN M, PADOVA C. Airfoil deflection characteristics during rub events[J]. Journal of Turbomachinery, 2012, 134: 011018-1-7.
    [15] 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): 1759-1799. 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): 1759-1799.
    [16] LEGRAND M, PIERRE C, PESEUX B. Structural modal interaction of a four degree of freedom bladed disk and casing model[J]. Journal of Computational and Nonlinear Dynamics, 2010, 5(4): 2040-2049.
    [17] 马辉,孙祺,太兴宇,等. 旋转叶片-机匣碰摩振动响应分析[J]. 振动与冲击, 2017, 36(14): 26-32. MA Hui, SUN Qi, TAI Xingyu, et al. Vibration response analysis of rotating blade-casing rubbing[J]. Journal of Vibration and Shock, 2017, 36(14): 26-32.
    [18] MA H, YIN F, TAI X, et al. Vibration response analysis caused by rubbing between rotating blade and casing[J]. Journal of Mechanical Science and Technology, 2016, 30(5): 1983-1995.

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