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轮盘端面齿连接的周向拉杆转子刚度研究
引用本文:李浦,袁奇,高进,谈芦益,李一峰,刘华峰.轮盘端面齿连接的周向拉杆转子刚度研究[J].航空动力学报,2013,28(7):1618-1623.
作者姓名:李浦  袁奇  高进  谈芦益  李一峰  刘华峰
作者单位:1. 西安交通大学能源与动力工程学院,西安,710049
2. 上海电气电站集团技术研究与发展中心,上海,201612
摘    要:针对轮盘端面齿连接的周向拉杆转子模型,理论分析得到转子各组成部分刚度计算方法.应用商业有限元软件ANSYS,基于三维有限元非线性接触算法计算预紧力下轮盘端面齿连接段的弯曲刚度和扭转刚度,得到刚度修正系数和刚度无量纲系数.分析周向拉杆刚度和轮盘刚度的关系,提出拉杆刚度比例系数.计算结果表明:刚度系数无量纲系数小于1时,刚度修正系数保持不变;刚度无量纲系数大于1时,此时预紧力不足,齿面发生滑移,刚度修正系数会突然降低,拉杆弯曲刚度比例系数会增加.刚度无量纲系数具有明确的物理意义,可为带端面齿的燃气轮机转子设计和故障诊断提供参考.

关 键 词:周向拉杆转子  端面齿  预紧力  有限元方法  刚度修正系数  刚度无量纲系数  拉杆刚度比例系数
收稿时间:2012/7/11 0:00:00

Investigation on stiffness of circumferential distributed tie-rod rotor with curvic couplings of trochal disk
LI Pu,YUAN Qi,GAO Jin,TAN Lu-yi,LI Yi-feng and LIU Hua-feng.Investigation on stiffness of circumferential distributed tie-rod rotor with curvic couplings of trochal disk[J].Journal of Aerospace Power,2013,28(7):1618-1623.
Authors:LI Pu  YUAN Qi  GAO Jin  TAN Lu-yi  LI Yi-feng and LIU Hua-feng
Institution:School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an 710049, China;School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an 710049, China;School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an 710049, China;Research and Development Center, Shanghai Electric Power Generation Group, Shanghai 201612, China;Research and Development Center, Shanghai Electric Power Generation Group, Shanghai 201612, China;Research and Development Center, Shanghai Electric Power Generation Group, Shanghai 201612, China
Abstract:Based on the circumferential distributed tie-rod rotor model with curvic couplings, the stiffness of every part of the rotor was acquired with analytical method. Three-dimensional finite element nonlinear contact method was adopted to analyse the flexural stiffness and torsional stiffness of the curvic couplings after preloading by using the commercial finite element software ANSYS. The stiffness correction coefficient and stiffness nondimensional coefficient were obtained. Coefficient of tie-rod stiffness ratio was adopted to describe the relation between the stiffness of tie-rods and disks. Results show that stiffness correction coefficient keeps steady when the stiffness nondimensional coefficient is less than 1, while it drops abruptly and the coefficient of tie-rod bend stiffness ratio increases when stiffness nondimensional coefficient exceeds 1. This means the preload is not enough and slip between curvic couplings happens. Stiffness nondimensional coefficient reflects some certain stress status of the curvic couplings, providing a basic guide for design and fault diagnosis of gas turbine rotor with curvic couplings.
Keywords:circumferential distributed tie-rod rotor  curvic couplings  preload  finite element method  stiffness correction factor  stiffness nondimensional coefficient  coefficient of tie-rod stiffness ratio
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