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同转/对转双转子系统的动力学特性
引用本文:蒋云帆,廖明夫,刘永泉,王德友,金路,鲁鹏.同转/对转双转子系统的动力学特性[J].航空动力学报,2013,28(12):2771-2780.
作者姓名:蒋云帆  廖明夫  刘永泉  王德友  金路  鲁鹏
作者单位:西北工业大学 动力与能源学院, 西安 710007;西北工业大学 动力与能源学院, 西安 710007;中国航空工业集团公司 沈阳发动机设计研究所, 沈阳 110015;中国航空工业集团公司 沈阳发动机设计研究所, 沈阳 110015;西北工业大学 动力与能源学院, 西安 710007;西北工业大学 动力与能源学院, 西安 710007
摘    要:建立了双转子动力学模型,引入中介轴承刚度和高、低压转子陀螺力矩的影响,利用数值分析和实验验证,揭示了同转/对转双转子系统临界转速特性和不平衡响应存在的差异,以及转速比对同转/对转双转子临界转速特性和不平衡响应的影响.结果表明:陀螺力矩是影响带有中介支承的双转子系统转子刚度的主要原因,其刚度变化与内、外转子的转速比大小和相对旋转方向有关,进而导致同转/对转双转子系统临界转速特性和不平衡响应发生改变;相比同结构的同转双转子,在相同的不平衡量作用下,对转双转子的不平衡响应更为显著.对转双转子进行动平衡时,应更加严格的控制内、外转子的不平衡量.

关 键 词:双转子  同转  对转  陀螺力矩  动力学特性
收稿时间:2012/11/15 0:00:00

Dynamic characteristics of co-rotating/counter-rotating dual-rotor system
JIANG Yun-fan,LIAO Ming-fu,LIU Yong-quan,WANG De-you,JIN Lu and LU Peng.Dynamic characteristics of co-rotating/counter-rotating dual-rotor system[J].Journal of Aerospace Power,2013,28(12):2771-2780.
Authors:JIANG Yun-fan  LIAO Ming-fu  LIU Yong-quan  WANG De-you  JIN Lu and LU Peng
Institution:School of Power and Energy, Northwestern Polytechnical University, Xi'an 710007;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710007;Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China, Shenyang 110015, China;Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China, Shenyang 110015, China;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710007;School of Power and Energy, Northwestern Polytechnical University, Xi'an 710007
Abstract:A dynamic model of dual-rotor was set up.The influence of inter-shaft bearing stiffness and the gyroscopic moments of high and low pressure rotors were considered in this model.The difference of co-rotating or counter-rotating dual-rotor's critical speed characteristics and unbalance response and the influence of speed ratio on co-rotating or counter-rotating dual-rotor's critical speed characteristics and unbalance response were revealed by numerical analysis and experiments.The results show that,gyroscopic moment is a main influential factor to the rotor stiffness of dual-rotor system with inter-shaft bearing,and the changes of stiffness are related to the speed ratio and the relative rotating direction of inner and outer rotors,further causing the change of co-rotating or counter-rotating dual-rotor's critical speed characteristics and unbalance response.Compared with the co-rotating dual-rotor of the same structure with the counter-rotating dual-rotor,the counter-rotating dual-rotor's unbalance response is more obvious than the co-rotating dual-rotor's under the same unbalance mass,and for this reason the unbalance mass of counter-rotating dual-rotor's inner and outer rotors should be controlled more strictly during the dynamic balance.
Keywords:dual-rotor  co-rotating  counter-rotating  gyroscopic moment  dynamic characteristic
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