套齿联轴器对航空发动机振动特性的影响

中国机械工程 ›› 2015, Vol. 26 ›› Issue (10): 1312-1319.

套齿联轴器对航空发动机振动特性的影响

廖仲坤1;陈果2;王海飞2

1.中国航天飞航技术研究院北京动力机械研究所,北京,100074
2.南京航空航天大学,南京,211106

出版日期:2015-05-25 发布日期:2015-05-26
基金资助:
国家自然科学基金资助项目（50705042）;航空科学基金资助项目（2007ZB52022）

Effects of Gear Coupling on Aero-engine Vibration Characteristics

Liao Zhongkun1;Chen Guo2;Wang Haifei2

1.Beijing Power Machine Research Institute,Aeronautics and Astronautics Technique Research Institute of China, Beijing,100074
2.Nanjing University of Aeronautics and Astronautics,Nanjing,211106

Online:2015-05-25 Published:2015-05-26
Supported by:
National Natural Science Foundation of China（No. 50705042）;Aviation Science Foundation of China（No. 2007ZB52022）

摘要/Abstract

摘要：

研究了航空发动机套齿联轴器的连接刚度，推导了套齿动态啮合力计算模型，分析了随扭矩、套齿不对中和动态相对位移变化的套齿啮合力和啮合刚度。依据航空发动机套齿连接结构，建立了含套齿联轴器的三支点转子动力学模型，分析了套齿连接刚度对系统频率响应特性的影响，在考虑转轴间角度不对中的情况下，分析了套齿连接刚度对系统不对中响应的影响规律。结果发现，动态啮合力模型能够更加真实地模拟套齿连接刚度的变化，但是，当其径向啮合刚度变化不大时，其计算结果与等效刚度模型的计算结果相同，套齿角向刚度对系统动力性能影响很大，在套齿设计、装配和使用中需要重视。

关键词: 航空发动机, 套齿联轴器, 啮合刚度, 不对中, 振动特性

Abstract:

The aero-engine gear coupling stiffness was studied herein,and the coupling dynamic gearing forces were deduced, the relationship among the gear coupling gearing forces and the torque, misalignment,and the dynamic relative displacements was analyzed. According to aero-engine gearing structure characteristics,a rotor dynamic model including gear coupling and the three supports was established,and the effects of gear coupling stiffness on the system frequency response function were analyzed; under the conditions of considering the angle misalignment between two rotors, the effects of gear stiffness on the misalignment responses were studied. The results show that the dynamic gearing stiffness model can simulate the gear coupling dynamic stiffness very correctly, but the dynamic change range of the stiffness is not enough to change obviously the system dynamic characteristics, however, the effects of the angle stiffness of gear coupling on the system vibration characteristics are very great.

Key words: aero-engine, gear coupling, gearing stiffness, misalignment, vibration characteristics

中图分类号:

V232

廖仲坤, 陈果, 王海飞. 套齿联轴器对航空发动机振动特性的影响[J]. 中国机械工程, 2015, 26(10): 1312-1319.

Liao Zhongkun, Chen Guo, Wang Haifei. Effects of Gear Coupling on Aero-engine Vibration Characteristics[J]. China Mechanical Engineering, 2015, 26(10): 1312-1319.

导出引用管理器 EndNote|Ris|BibTeX

链接本文: https://www.cmemo.org.cn/CN/

https://www.cmemo.org.cn/CN/Y2015/V26/I10/1312

参考文献

[1]航空发动机设计手册总编委会.航空发动机设计手册(第19分册)转子动力学及整机振动[M].北京:航空工业出版社,2000.
[2]刘占生,赵广,龙鑫.转子系统联轴器不对中研究综述[J].汽轮机技术,2007,49(5):321-325.
[3]韩捷,石来德.转子系统齿式联接不对中故障的运动学机理研究[J].振动工程学报,2004,17(4):416-420.
[4]陈果,李兴阳.航空发动机整机振动中的不平衡-不对中-碰摩耦合故障研究[J].航空动力学报,2009(10).
[5]龙鑫.齿式联轴器不对中动力学特性研究[D].哈尔滨工业大学,2006:
[6]赵广.转子—联轴器—轴承—隔振器系统耦合动力学特性研究[D].哈尔滨工业大学,2009:
[7]Lee Y S, Lee C W. Modelling and Vibration Analysis of Misaligned Rotor-ball Bearing Systems[J]. Journal of Sound and Vibration, 1999,224 (1) : 17- 32.
[8]Ai-Hussain K M, Redmond I. Dynamic Response of Two Rotors Connected by Rigid Mechanical Coupiing with Parallel Misalignment[J]. Journal of Sound and Vibration,2002,249(1) 483-498.
[9]A1-Hussain K M, Redmond I. Dynamic Stability of Two Rigid Rotors Connected by a Flecible Coupling with Augular Misalignment[J]. Journal of Sound and Vibration, 2003,266 (2) : 217-234.
[10]Li M, Yu L. Analysis of the Coupled Lateral Vibration of a Rotor-bearing-system with a Misaligned Gear Coupling[J]. Journal of Sound and Vibration, 2001,243 (2) : 283-300.
[11]李明.齿轮联轴器不对中转子系统的稳态振动特征分析[J].机械强度,2002,24(1):52-55.
[12]陈果.双转子航空发动机整机振动建模与分析[J].振动工程学报,2011,24(6):619-632.
[13]陈果.航空发动机整机振动耦合动力学模型及其验证[J].航空动力学报,2012,27(2):241-254.
[14]Xu M, Marangoni R D Motor- flexible Coupling Vibration Analysis of a rotor System Subject to Misalignment and Unbalance, PART I: Theoretical Model and Analysis[J] Journal of Sound and Vibration, 1994, 176(5): 663-679.
[15]Xu M, Marangoni R D. Vibration Analysis of a Motor-flexible Coupling-rotor System Subject to Misalignment and Unbalance, PART II : Experimental Validation[J]. Journal of Sound and Vibration, 1994,176 (5) : 681-691.