Volume 30 Issue 4
Apr.  2015
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Article Navigation >  Journal of Aerospace Power  > 2015  >  30(4): 952-965
CHEN Guo, WANG Hai-fei, LIU Yong-quan, FENG Guo-quan, JIANG Guang-yi, LI Cheng-gang, WANG De-you. A new blade-casing rubbing model and its verification[J]. Journal of Aerospace Power, 2015, 30(4): 952-965. doi: 10.13224/j.cnki.jasp.2015.04.023
Citation: CHEN Guo, WANG Hai-fei, LIU Yong-quan, FENG Guo-quan, JIANG Guang-yi, LI Cheng-gang, WANG De-you. A new blade-casing rubbing model and its verification[J]. Journal of Aerospace Power, 2015, 30(4): 952-965. doi: 10.13224/j.cnki.jasp.2015.04.023
shu

A new blade-casing rubbing model and its verification

doi: 10.13224/j.cnki.jasp.2015.04.023

  • 1. College of Civil Aviation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

  • 2. Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China, Shenyang 110015, China

  • Received Date: 2013-11-07
  • Publish Date: 2015-04-28
    Abstract
  • For the aero-engine blade-casing rubbing fault, a new blade-casing rubbing model was put forward. On the basis of tranditional elastic rubbing model, the new model considerd the effects of blade number and the rotor-stator clearance change on rubbing forces, and it could simulate rubbing faults with various rubbing positions including single-point, multi-points, part and whole-cycle on casing and rotor. The new rubbing model was applied to the rotor-support-casing coupling dynamic model, and the casing acceleration responses under rubbing faults were obtained by the numerical integration approach. The aero-engine rotor tester including casing was used to carry out the rubbing test whose rubbing positions were the single-point on casing and whole-cycle on rotor, and it is found that the rubbing characteristics of the casing vibration acceleration signals have obvious periodic impact characteristics. The impact frequency is the frequency of the blades passing the casing, which equals to the product of the rotational frequency and blade number. There is a blade passing frequency and its multiple-frequency components in the high-frequency band of spectrum, and the impact is modulated by the rotational frequency. There are obvious quefrency components of rotational frequency components and its multiple frequencies in the signal cepstrum.The simulation results agree well with the test values, and the new blade-casing rubbing model is fully verified. Finnaly, based on the new blade-casing rubbing model, the other rubbing modes between rotor and casing were simulated, and the casing vibration charateristics were obtained.

     

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    • References(26)
  • [1]
    Beatty R F.Differentiating rotor response due to radial rubbing[R].Journal of Vibration, Acoustics, Stress and Reliability in Design, 1985, 107(2):151-160.
    [2]
    Li G X, Paidoussics M P.Impact phenomena of rotor-casing dynamic system[J].Nonlinear Dynamics, 1994, 5(1):53-70.
    [3]
    张思进, 陆启韶, 王琪.转子与定子几何不对中引起的碰摩分析[J].振动工程学报, 1998, 11(4):492-496. ZHANG Sijin, LU Qishao, WANG Qi.Analysis of rub-impact events for a rotor eccentric from the case[J].Journal of Vibration Engineering, 1998, 11(4):492-496.(in Chinese)
    [4]
    刘献栋.旋转机械转静件碰摩故障及其诊断技术的研究[D].北京:北京航空航天大学, 1999. LIU Xiandong.Study on rotor-stator rubbing fault and its diagnosis technique in rotating machine[D].Beijing:Beijing University of Aeronautics and Astronautics, 1999.(in Chinese)
    [5]
    褚福磊, 马正松, 冯冠平.碰摩转子系统的混沌特征[J].清华大学学报:自然科学版, 1996, 36(7):52-57. CHU Fulei, MA Zhengsong, FENG Guanping.Chaotic behavior of a rub rotor model[J].Journal of Tsinghua University:Science and Technology, 1996, 36(7):52-57.(in Chinese)
    [6]
    Chen G, LI C G, Wang D Y.Nonlinear dynamic analysis and experiment verification of rotor-ball bearings-support-stator coupling system for aeroengine with rubbing coupling faults[J].Journal of Engineering for Gas Turbines and Power, 2010, 132(2):022501.1-022501.9.
    [7]
    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 aero-engine blade-to-case rub-impact[J].Journal of Aerospace Power, 2011, 26(6):1282-1288.(in Chinese)
    [8]
    Williams R J.Simulation of blade casing interaction phenomena in gas turbines resulting from heavy tip rubs using an implicit time marching method[R].ASME Paper GT2011-45495, 2011
    [9]
    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.
    [10]
    Turner K M, Dunn A M.Simulation of engine blade tip-rub induced vibration[R].ASME Paper GT2005-68217, 2005.
    [11]
    Turner K E, Dunn M, Padova M.Airfoil deflection characteristics during rub events[R].ASME Paper GT2010-22166, 20100.
    [12]
    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):1756-1761. TAI Xingyu, MA Hui, TAN Zhen, et al.Research and numerical simulation on dynamic characteristics of blade-casing with impulse loading[J].Journal of Northeastern University:Natural Science, 2012, 33(12):1756-1761.(in Chinese)
    [13]
    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):13-41.
    [14]
    Batailly A, Legrand M, Cartraud P, et al.Assessment of reduced models for the detection of modal interaction through rotor stator contacts[J].Journal of Sound and Vibration, 2010, 329(26):5546-5562.
    [15]
    Legrand M, Barailly 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(11):011010.1-011010.11.
    [16]
    Padovan J, Choy F K.Nonlinear dynamics of rotor/blade/casing rub interactions[J].Journal of Turbomachinery, 1987, 109(4):527-534.
    [17]
    Sinha S K, Ojha S.Rotordynamic analysis of asymmetric turbofan rotor due to fan blade-out event with contact-impact rub loads[J].Journal of Sound and Vibration, 2013, 332(9):2253-2283.
    [18]
    Ehrich F F.High order subharmonic response of high speed rotors in bearing clearance[J].Journal of Vibration, Acoustics, Stress and Reliability in Design, 1988, 110(1):9-16.
    [19]
    晏砺堂, 王德友.航空双转子发动机动静件碰摩振动特征研究[J].航空动力学报, 1998, 13(2):173-176. YAN Litang, WANG Deyou.Vibration features from rubbing between rotor and casing for a dual-shaft aero-engine[J].Journal of Aerospace Power, 1998, 13(2):173-176.(in Chinese)
    [20]
    周海仑, 陈果.航空发动机双转子-滚动轴承-机匣耦合系统动力学分析[J].航空动力学报, 2009, 24(6):1284-1290. ZHOU Hailun, CHEN Guo.Dynamic response analysis of dual rotor-ball bearing-stator coupling system for aero-engine[J].Journal of Aerospace Power, 2009, 24(6):1284-1290.(in Chinese)
    [21]
    袁惠群, 贺威, 韩清凯.发动机双转子-机匣耦合系统碰摩故障分析[J].航空动力学报, 2011, 26(11):2401-2408. YUAN Huiqun, HE Wei, HAN Qingkai.Analysis on rubs of double rotor-stator coupling system[J].Journal of Aerospace Power, 2011, 26(11):2401-2408.(in Chinese)
    [22]
    宋友, 柳重堪, 李其汉.基于小波变换的转子动静件碰摩故障诊断研究[J].振动工程学报, 2002, 15(3):200-207. SONG You, LIU Chongkan, LI Qihan.Research on rub-impact fault between rotor and stator using wavelet trans form[J].Journal of Vibration Engineering, 2002, 15(3):200-207.(in Chinese)
    [23]
    何田, 刘献栋, 李其汉.噪声背景下检测突变信息的奇异值分解技术[J].振动工程学报, 2006, 19(3):399-403. HE Tian, LIU Xiandong, LI Qihan.An improved method of detecting abrupt information based on singularity value decomposition in noise background[J].Journal of Vibration Engineering, 2006, 19(3):399-403.(in Chinese)
    [24]
    何田, 刘献栋, 李其汉.改进的Hilbert-Huang变换及其在转静子碰摩仿真中得应用[J].航空动力学报, 2007, 22(10):1779-1784. HE Tian, LIU Xiandong, LI Qihan.Improved Hilbert-Huang transform and its application in rotor-stator rub[J]Journal of Aerospace Power, 2007, 22(10):1779-1784.(in Chinese)
    [25]
    王美令, 陈果.基于关联维数和小波能量谱熵的碰摩故障智能诊断[J].振动与冲击, 2010, 29(8):174-177, 197. WANG Meiling, CHEN Guo.Based on correlation dimension and wavelet energy spectrum entropy rubbing intelligent fault diagnosis[J].Journal of Vibration and Shock, 2010, 29(8):174-177, 197.(in Chinese)
    [26]
    陈果.航空发动机整机振动耦合动力学新模型及其验证[J].航空动力学报, 2012, 27(2):241-254. CHEN Guo.A coupling dynamic model for whole aero-engine vibration and its verification[J].Journal of Aerospace Power, 2012, 27(2):241-254.(in Chinese)
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