[1] 洪杰,于欢,肖森,等.高速柔性转子系统非线性振动响应特征分析[J].北京航空航天大学学报,2018,44(4):653-661.HONG J,YU H,XIAO S,et al.Nonlinear vibration response characteristics of high-speed flexible rotor system[J].Journal of Beijing University of Aeronautics and Astronautics,2018,44(4):653-661(in Chinese).
[2] 于欢,马艳红,肖森,等.高速柔性转子支承松动力学特征及动力特性[J].北京航空航天大学学报,2017,43(8):1677-1683.YU H,MA Y H,XIAO S,et al.Mechanical and dynamic characteristics of bearing with looseness on high-speed flexible rotor[J].Journal of Beijing University of Aeronautics and Astronautics,2017,43(8):1677-1683(in Chinese).
[3] 廖明夫,刘永泉,王四季,等.中介轴承对双转子振动的影响[J].机械科学与技术,2013,32(5):641-646.LIAO M F,LIU Y Q,WANG S J,et al.The vibration features of a twin spool rotor system with an inter-bearing[J].Mechanical Science and Technology for Aerospace Engineering,2013,32(5):641-646(in Chinese).
[4] 王俨剀,廖明夫,张家豪.航空发动机中介轴承的动力学减载设计[J].航空动力学报,2017,32(2):492-499.WANG Y K,LIAO M F,ZHANG J H.Dynamic load reduction design for inter-shaft bearing of aircraft engine[J].Journal of Aerospace Power,2017,32(2):492-499(in Chinese).
[5] CHILDS D W.A modal transient rotor dynamic model for dual-rotor jet engine systems[J].Journal of Manufacturing Science and Engineering,1976,98(3):876-882.
[6] GUPTA K,ATHRE K,GUPTA K D.Unbalance response of a dual rotor system:Theory and experiment[J].Journal of Vibration and Acoustics,1993,115(4):427-435.
[7] GUPTA K D,GUPTA K,ATHRE K.Stability analysis of dual rotor system by extended transfer matrix method[C]//ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition.New York:ASME,1989:V005T13A013.
[8] LI Q,YAN L,HAMILTON J F.Investigation of the steady-state response of a dual-rotor system with intershaft squeeze film damper[J].Journal of Engineering for Gas Turbines and Power,1985,108(4):613-618.
[9] HYLTON P D.Minimizing dynamic response of counter-rotating engines through optimized node placement[C]//ASME Turbo Expo 2010.New York:ASME,2010:25-32.
[10] CHEN X,LIAO M F.Steady-state characteristic of a dual-rotor system with intershaft bearing subjected to mass unbalance and base motions:GT-2018-75215[R].New York:ASME,2018.
[11] CHEN X,LIAO M F.Transient characteristic of a dual-rotor system with intershaft bearing subjected to mass unbalance and base motions dueing start-up:GT-2018-75227[R].New York:ASME,2018.
[12] YU P C,ZHANG D Y,MA Y H,et al.Dynamic modeling and vibration characteristics analysis of the aero-engine dual-rotor system with fan blade out[J].Mechanical Systems and Signal Processing,2018,106:158-175.
[13] 钟一谔,何衍宗,王正,等.转子动力学[M].北京:清华大学出版社,1984.ZHONG Y E,HE Y Z,WANG Z,et al.Rotor dymamics[M].Beijing:Tsinghua University Press,1984(in Chinese).
[14] 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,2015,36(2):292-298.ZHANG D Y,LIU Y H,LIANG Z C,et al.Prediction for critical speed of double spools system in aero engines[J].Journal of Propulsion Technology,2015,36(2):292-298(in Chinese).
[15] 洪杰,王华,肖大为,等.转子支承动刚度对转子动力特性的影响分析[J].航空发动机,2008,34(1):23-27.HONG J,WANG H,XIAO D W,et al.Effects of dynamic stiffness of rotor bearing on rotor dynamic characteristics[J].Aeroengine,2008,34(1):23-27(in Chinese).
[16] 马艳红,何天元,张大义,等.支承刚度非线性转子系统的不平衡响应[J].航空动力学报,2014,29(7):1527-1534.MA Y H,HE T Y,ZHANG D Y,et al.Imbalance response of rotor system with nonlinear bearing stiffness[J].Journal of Aerospace Power,2014,29(7):1527-1534(in Chinese). |