Effect of asymmetrical supports on the dynamic characteristics of a dual-rotor system
WANG Jie1,ZUO Yanfei1,JIANG Zhinong2,FENG Kun2,HU Minghui3,ZHANG Wenhai3
1.Key Lab of Engine Health Monitoring-Control and Networking of Ministry of Education, Beijing University of Chemical Technology, Beijing 100029, China;
2.Beijing Key Laboratory of High-end Mechanical Equipment Health Monitoring and Self-Recovery, Beijing University of Chemical Technology, Beijing 100029, China;
3.Aero Engine Vibration Health Monitoring-Control Joint Lab, AVIC Shenyang Engine Design Institute-Beijing University of Chemical Technology, Beijing 100029,China
Abstract:The asymmetry of support stiffness widely exists in the rotor support system. However, the complex influence of asymmetric support on the dynamic characteristics of the dual-rotor system in engineering is not clear. For this reason, the dual-rotor support system with typical engine rotating in the same direction is taken as the research object. According to the characteristics of the thin-walled flexible casing support of the engine, the index of support asymmetry coefficient is proposed, and the effects of the existence of support asymmetry and its variation on the critical speed, steady-state unbalance response, whirling direction and whirling trajectory of the dual-rotor support system are studied. It is found that the asymmetry of the support will lead to the increase of the forward critical speed and the decrease of the backward critical speed corresponding to the relevant modes. The response peak of some pivots appears near the critical speed of whirling and it is accompanied by the change of vibration phase in the whirling plane. The whirling of the rotor is more complex. The forward and backward whirling occur simultaneously on the same rotor, and the whirling trajectory of the specific node of the rotor will change more complex with the rotational speed. Further study shows that the increase of the asymmetric coefficient will result in an overall increase in the speed and position regions where the backward whirling occurs, but the area of the backward whirling may also decrease in the specific speed or position. The obtained influence can provide reference for the dynamic design of engine dual-rotor system under complex support conditions and the explanation of the special vibration phenomena.
王杰1,左彦飞1,江志农2,冯坤2,胡明辉3,张文海3. 支承非对称对双转子系统动力特性的影响规律[J]. 振动与冲击, 2020, 39(18): 27-33.
WANG Jie1,ZUO Yanfei1,JIANG Zhinong2,FENG Kun2,HU Minghui3,ZHANG Wenhai3. Effect of asymmetrical supports on the dynamic characteristics of a dual-rotor system. JOURNAL OF VIBRATION AND SHOCK, 2020, 39(18): 27-33.
[1] Smith D. M. The Motion of a Rotor Carried by a Flexible Shaft in Flexible Bearings[J]. Proceedings of the Royal Society of London, 1933, 142(846): 92-118
[2] Biezeno C. B. Translat. Engineering dynamics[M]. Blackie, 1954
[3] Downham E. Theory of Shaft Whirling No. 5 - The Influence of Plain Bearings on Shaft Whirling[J]. Engineer, 1957: 10
[4] 方之楚, 骆振黄. 各向异性支承中的单盘转子过临界点时的瞬态响应[J]. 固体力学学报, 1987(04): 321-330
Fang Zhichu, Luo Zhenhuang. Transient Response of a Sin-gle Disk Rotor in Anisotropic Bearings at the Critical Point[J]. Chinese Journal of Solid Mechanics, 1987(04): 321-330
[5] Lee C. W. Vibration Analysis of Rotors[M]. Kluwer Academic Publishers, 1993: 511-511
[6] Wang Shuai, Wang Yu, Y. Zi. A 3D Finite Element-Based Model Order Reduction Rotor-Bearing Systems[J]. Journal of Sound & Vibration, 2015, 359: 116-135
[7] Nelson H. D. The Dynamics of Rotor Bearing Systems, Using Finite Elements[J]. Transactions of the American Society Mechanical Engineers Journal of Engineering for Industry. 1976, 98(2): 593
[8] Nonami K. Response in Passing Through Critical Speed of Arbitrarily Distributed Flexible Rotor System : Part 2,Case with Gyroscopic Effect[J]. Bulletin of Jsme. 2008, 2 (217): 1205-1212
[9] Joh C. Y., Lee C. W. Use of dFRFs for Diagnosis of Asymmetric/Anisotropic Properties in Rotor-Bearing System[J]. Journal of Vibration & Acoustics, 1996, 118 (1): 26-29
[10] Han D. J. Generalized Modal Balancing for Non-Isotropic Rotor Systems[J]. Mechanical Systems & Signal Processing. 2007, 21(5): 2137-2160
[11] Fei Z. X, Tong S. G, Wei C. Investigation of the Dynamic Characteristics of a Dual-Rotor System and its start-up Simulation Based on Finite Element Method[J]. Journal of Zhejiang University-Science A(Applied Physics & Engineering), 2013, 14 (4): 268-280
[12] 张大义, 刘烨辉, 梁智超, 等. 航空发动机双转子系统临界转速求解方法[J]. 推进技术, 2015 (02): 292-298
Zhang Dayi, Liu Yehui, Liang Zhichao, et al. Method for Solving Critical Speed of Aeroengine Dual-Rotor System[J]. Propulsion Technology, 2015 (02): 292-298
[13] Ferraris G., Maisonneuve V., Lalanne M. Prediction of the dynamic behavior of non-symmetrical coaxial co-or counter-rotating rotors[J]. Journal of Sound & Vibration. 1996, 195 (4):649-666
[14] 左彦飞. 航空发动机整机系统结构振动分析[D]. 北京: 北京航空航天大学, 2016.
Zuo Yanfei. Structural dynamic analysis of the whole aero-engine system[D]. Beijing: Beihang University, 2016.
[15] Ma W. M, Wang J. J. 3D Solid Finite Element Modeling and Rotordynamics of Large Rotating Machines: Application to an Industrial Turbo Engine[J]. Advanced Materials Research, 2012, 591-593:1879-1885