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柔性转子无试重模态动平衡测试系统 被引量:7

Development of Modal Balancing System Without Trail Weights for High Speed Flexible Rotors
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摘要 针对传统柔性转子动平衡方法需要多次添加试重、多次启动而导致平衡效率低、安全性无法保证的问题,提出了一种高速柔性转子无试重模态动平衡方法。该方法借助有限元软件计算得到转子的模态特征,结合测量得到的振动信息,计算出平衡配重的大小和相位。为了将此方法应用于工程实际,研制了一套柔性转子无试重模态动平衡软、硬件测试系统。将该系统与国外同类先进测试设备SIRIUS对比,两者之间的相位测量误差为2.376°。转速计量表明,该测试系统的转速测量范围为0~60kr/min,最大测量误差为10%。应用该系统对跨二阶双盘柔性转子实施了无试重动平衡试验,平衡后一阶振幅下降60.6%,二阶振幅下降74%。试验结果表明,所研制的无试重模态动平衡系统可有效应用于高速柔性转子的动平衡,提高平衡效率和安全性。 Traditional methods of flexible rotor balancing need to add trail weights and run the rotor many times,resulting in a low balancing efficiency and a poor security.To solve this problem,a modal balancing method for high speed flexible rotor without trail weights is proposed.Modal information is obtained by finite element software and vibration data are measured to calculate the size and orientation of the unbalance mass.In order to easily and comfortably apply this method to engineering practice,a balancing system corresponding to the proposed method is developed,including software and hardware.The phase measurement error between the system and similar foreign advanced testing equipment SIRIUS is 2.376°.Further,the results of rotationspeed calibrationshows the measurement range of the system is 0~60 kr/min with an error less than 10%.Finally,a two-disk flexible rotor across the second order critical speed is balanced using the system.After balancing,the amplitude of the rotor at the first order critical speed reduces by 60.6%,the amplitude at the second order critical speed reduces by 74%.The results demonstrate that the system can be effectively applied to perform flexible rotor balancing,improving the efficiency and safety of balancing.
作者 贾胜锡 郑龙席 邓旺群 梅庆 JIA Shengxi;ZHENG Longxi;DENG Wangqun;MEI Qin(College of Power and Energy,Northwestern Polytechnical University,Xi’an,710072,China;College of Power and Energy,Northwestern Polytechnical University,Xi’an,710072,China;Aviation Key Laboratory of Aeroengine Vibration Technology,AECC Hunan Powerplant Research Institute,Zhuzhou,412002,China)
出处 《振动.测试与诊断》 EI CSCD 北大核心 2018年第6期1108-1113,1287,1288,共8页 Journal of Vibration,Measurement & Diagnosis
基金 航空科学基金资助项目(20112153019)
关键词 柔性转子 试重 模态动平衡 LABWINDOWS/CVI 采样率 flexible rotor trail weights modal balance LabWindows/CVI sampling rate
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  • 1邓旺群,高德平,刘金南,雷沫枝.转子高速动平衡技术在涡轴发动机整机减振中的作用[J].航空动力学报,2005,20(1):78-85. 被引量:19
  • 2邓旺群,高德平.悬臂柔性转子动力特性及高速动平衡试验[J].航空动力学报,2006,21(3):556-562. 被引量:14
  • 3闻邦椿,顾家柳,夏松波,等.高等转子动力学:理论、技术与应用[M].北京:机械工业出版社,1999.
  • 4尹泽勇,付才高,李其汉,等.《航空发动机设计手册》第19册-转子动力学及整机振动[M].北京:航空工业出版社,2000:1-7.
  • 5Palazzolo A B, Gunter E J. Modal balancing of a multi-mass flexible rotor without trial weights [R]. New York: [s. n.], 1982.
  • 6Wiese D. Two new procedures to balance flexible ro tors without test runs [C]//Proceedings of the 5th In ternational Conference on Vibrations in Rotating Ma chinery. London: [s. n. ], 1992: 557-568.
  • 7Kreuzinger J T, Irretier H. Unbalance identi? cation of flexible rotors based on experimental modal analysis [C] // Proceedings of the 7th International Conference on Vibrations in Rotating Machinery. London: [s. n.], 2000: 335-346.
  • 8Tan S G , Wang X X. A theoretical introduction to low speed balancing of flexible rotors., unification and development of the modal balancing and influence coefficient techniques [J]. Journal of Sound and Vibrations, 1993, 168(3): 385-394.
  • 9郑龙席,李晓丰,刘振侠.一种高速柔性转子动平衡方法:中国,201010284567[P].2011-01-19.
  • 10Gupta K,Singh S P.Damping measurements in fiber reinforced composite rotors [J].Indian Institute of Technology,1998,211(3):513-520.

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