[1] 廖明夫.航空发动机转子动力学[M].西安:西北工业大学出版社,2015.
[2] 杨丹,甘春标,杨世锡,等.一类初弯曲转子的裂纹-碰摩故障响应分析[J].浙江大学学报(工学版),2014,48(8):1496-1501.
[3] BENTLY D E,CHARLES T H.Fundamentals of Rotating Machinery Diagnostics[M].Minden,NV,USA:Bently Pressurized Bearing Press,2002.
[4] 窦唯,叶志明,闫宇龙.涡轮泵叶轮/转子配合间隙对稳定性的影响[J].火箭推进,2016,42(4):26-34.DOUW,YE Z M,YAN Y L.Effect of tolerance clearance between turbine rotor and impeller in liquid-propellant rocket engine on stability[J].Journal of Rocket Propulsion,2016,42(4):26-34.
[5] 吴文青,谢诞梅,杨毅,等.具有初始弯曲的1 000 MW汽轮机低压转子的振动特征分析[J].振动与冲击,2014,33(17):150-153,166.
[6] KEOGH P S,MORTON P G.The dynamic nature of rotor thermal bending due to unsteady lubricant shearing within a bearing[J].Proceedings of the Royal Society A:Mathematical,Physical and Engineering Sciences,1994,445(1924):273-290.
[7] 邹剑,董广明,陈进.含初始弯曲裂纹转子的振动分析[J].振动与冲击,2012,31(3):153-156.
[8] 王魁.涡轮泵转子动平衡的控制方法研究[J].火箭推进,2002,28(6):15-18.WANG K.Study on control method of rotor dynamic balance of turbine pump [J].Journal of Rocket Propulsion,2002,28(6):15-18.
[9] KANG C H,HSU W C,LEE E K,et al.Dynamic analysis of gear-rotor system with viscoelastic supports under residual shaft bow effect[J].Mechanism and Machine Theory,2011,46(3):264-275.
[10] 沈小要,贾九红,赵玫.具有初始弯曲的不平衡转子碰摩条件的研究[J].振动与冲击,2007,26(9):11-13.
[11] 郭小鹏,吴英祥,姜广义.转子热弯曲引起的振动故障特征与试验研究[J].沈阳航空航天大学学报,2015,5(32):26-31.
[12] 王静,郭九梅,王胤龙.离心压缩机转子弯曲故障分析[J].风机技术,2009,51(6):75-77.
[13] LIN F S,MENG G.Dynamic characteristics of an unbalanced rotor with asymmetric rigidity and initial bending[C]//Proceedings of the Asia-Pacific Vibration Conference.Hangzhou:[s.n.],2001.
[14] TONG X M,PALAZZOLO A.Tilting pad gas bearing induced thermal bow- rotor instability(Morton effect)[J].Tribology International,2018,121:269-279.
[15] RAO J S.History of rotating machinery dynamics[M].Netherlands:Springer,2011.
[16] 顾家柳,丁奎元,刘启洲,等.转子动力学[M].北京:国防工业出版社,1985.