1. 国能南京电力试验研究有限公司,南京,210000
2. 东方电气集团东方汽轮机有限公司,四川,德阳,618000
3. 西安交通大学叶轮机械研究所,西安,710049
: 2023-11-07。作者简介: 殷戈(1983—),男,高级工程师
李志刚(通信作者),男,教授,博士生导师。基金项目: 国家自然科学基金资助项目(52176042)
网络首发:2024-06-10,
纸质出版:2024
移动端阅览
殷戈, 黄彪, 黄新长, 等. 具有前置凸台防旋板的汽轮机交错齿迷宫密封动力学特性研究[J]. 西安交通大学学报, 2024,58(6):53-64.
YIN Ge, HUANG Biao, HUANG Xinchang, et al. Study on Rotordynamic Characteristics of the Staggered-Tooth LabyrinthSeal Mounting Anti-Swirl Brake with Upstream Rotor-Step in Steam Turbines[J]. 2024, 58(6): 53-64.
殷戈, 黄彪, 黄新长, 等. 具有前置凸台防旋板的汽轮机交错齿迷宫密封动力学特性研究[J]. 西安交通大学学报, 2024,58(6):53-64. DOI: 10.7652/xjtuxb202406006.
YIN Ge, HUANG Biao, HUANG Xinchang, et al. Study on Rotordynamic Characteristics of the Staggered-Tooth LabyrinthSeal Mounting Anti-Swirl Brake with Upstream Rotor-Step in Steam Turbines[J]. 2024, 58(6): 53-64. DOI: 10.7652/xjtuxb202406006.
为提高汽轮机多级轴端迷宫密封动力学性能
针对汽轮机两级轴端交错齿迷宫密封
开展了具有前置凸台的新型防旋板结构方案设计和止旋抑振性能评估。首先
针对两级轴端交错齿迷宫密封
设计了一级和两级传统防旋板、一级和两级前置凸台新型防旋板等动密封防旋板结构方案
并建立了具有“虚拟旁路边界”的有、无防旋板多级交错齿迷宫密封动力学计算模型
实现了对多级动密封进口压力场和高预旋速度场的精准模拟; 然后
采用基于多频椭圆轨迹涡动模型的动密封气流激振动力学特性(CFD)摄动数值预测方法
对比分析了无防旋板、传统防旋板和新型前置凸台防旋板作用下
两级交错齿迷宫密封泄漏特性和气流激振动力学特性; 最后
通过分析不同防旋板结构方案下
两级交错齿迷宫密封腔室旋流发展、腔室速度场和动态压力分布、转子面气流激振力
阐明了防旋板的止旋抑振机制。结果表明:无防旋板的迷宫密封具有最低的泄漏量
一级传统防旋板或一级前置凸台防旋板的设置会使密封齿数减少
导致密封泄漏量增加约4.5%; 相比于一级防旋板
具有两级防旋板的迷宫密封泄漏量增加约5.5%; 相比于传统防旋板
前置凸台防旋板可减小交叉刚度、增大有效阻尼; 相比于一级防旋板
两级防旋板可减小高涡动频率下的交叉刚度、增大直接阻尼
进而提高密封的有效阻尼; 在传统防旋板的基础上设置前置凸台可提升防旋板的止旋性能
且两级防旋板可有效抑制密封下游区域的旋流发展
能显著提升迷宫密封动力学性能、抑制汽轮机轴系振动失稳。
To improve the dynamic performance of multi-stage labyrinth seal on turbine shaft
the structure design and performance evaluation of anti-swirl and vibration suppression are proposed for a new type of anti-swirl brake with upstream rotor-step in two-stage labyrinth seal with staggered teeth. Firstly
four types of anti-swirl brakes for two-stage staggered-tooth labyrinth seal are designed in this paper. In addition
a dynamic calculation model of labyrinth seal with “virtual bypass boundary” is established to achieve accurate simulation in the pressure field and high swirl velocity field. Then
a transient computational fluid dynamic CFD-based perturbation method based on the multiple-frequency elliptical-orbit rotor whirling model is adopted to analyze the leakage characteristics and dynamic characteristic coefficients of labyrinth seal with various anti-swirl brakes. Finally
the performance of anti-swirl and vibration suppression is elucidated by analyzing swirl velocity development
velocity field and dynamic pressure distribution of labyrinth seal. The results show that the labyrinth seal without anti-swirl brake has the lowest leakage
and the addition of the one-stage traditional anti-swirl brake or the one-stage anti-swirl brake with upstream rotor-step will reduce the number of seal teeth
resulting in the increase of seal leakage(by about 4.5%). Compared with the one-stage anti-swirl brake
the two-stage anti-swirl brake can further increase the leakage by 5.5%. Compared with the traditional anti-swirl brake
the swirl brake with upstream rotor-step can decrease cross-coupled stiffness and increase the effective damping. Compared with the one-stage anti-swirl brake
the cross-coupled stiffness of two-stage anti-swirl brake can be further reduced and the direct damping can be increased
so the effective damping can be significantly increased. Installing the upstream rotor-step on the basis of the traditional anti-swirl brake can improve the anti-swirl performance and two-stage anti-swirl brake can effectively suppress the development of swirl in the downstream of the seal. The research results show that compared with the one-stage anti-swirl brake
the multi-stage anti-swirl brake has better performance of improving the dynamic characteristics and suppressing the vibration.
CHUPP R E, HENDRICKS R C, LATTIME S B, et al. Sealing in turbomachinery [J]. Journal of Propulsion and Power, 2006, 22(2): 313-349.
GAO Rui. Computational fluid dynamic and rotordynamic study on the labyrinth seal [D]. Blacksburg, USA: Virginia Polytechnic Institute and State University, 2012.
李军, 晏鑫, 丰镇平, 等. 透平机械阻尼密封技术及其转子动力特性研究进展 [J]. 热力透平, 2009, 38(1): 5-9.
LI Jun, YAN Xin, FENG Zhenping, et al. State-of-the art of turbomachinery damper seals technology and their rotordynamic characteristics [J]. Thermal Turbine, 2009, 38(1): 5-9, 14.
PINEAU G, ZERARKA A, ARGHIR M. Rotordynamic analysis of textured annular seals with multiphase(bubbly)flow [J]. INCAS Bulletin, 2011, 3(3): 3-13.
王天昊, 李志刚, 李军. 采用Bulk-Flow模型的直通式迷宫密封转子动力特性研究 [J]. 西安交通大学学报, 2021, 55(5): 25-33.
WANG Tianhao, LI Zhigang, LI Jun. Investigation on the rotordynamic characteristics of straight-through labyrinth seal using Bulk-Flow model [J]. Journal of Xi'an Jiaotong University, 2021, 55(5): 25-33.
YAN Xin, LI Jun, FENG Zhenping. Investigations on the rotordynamic characteristics of a hole-pattern seal using transient CFD and periodic circular orbit model [J]. Journal of Vibration and Acoustics, 2011, 133(4): 041007.
LI Zhigang, LI Jun, YAN Xin. Multiple frequencies elliptical whirling orbit model and transient RANS solution approach to rotordynamic coefficients of annual gas seals prediction [J]. Journal of Vibration and Acoustics, 2013, 135(3): 031005.
NIELSEN K K, CHILDS D W, MYLLERUP C M. Experimental and theoretical comparison of two swirl brake designs [J]. Journal of Turbomachinery, 2001, 123(2): 353-358.
CHILDS D W, SCHARRER J K. Experimental rotordynamic coefficient results for teeth-on-rotor and teeth-on-stator labyrinth gas seals [J]. Journal of Engineering for Gas Turbines and Power, 1986, 108(4): 599-604.
陈尧兴, 李志刚, 李军. 进口预旋对高压迷宫密封流体激振转子动力特性的影响 [J]. 润滑与密封, 2017, 42(11): 1-6.
CHEN Yaoxing, LI Zhigang, LI Jun. Effects of inlet preswirl on the flow excitation rotordynamic characteristics of labyrinth seal [J]. Lubrication Engineering, 2017, 42(11): 1-6.
LI Zhigang, LI Jun, FENG Zhenping.Numerical comparison of rotordynamic characteristics for a fully partitioned pocket damper seal and a labyrinth seal with high positive and negative inlet preswirl [J]. Journal of Engineering for Gas Turbines and Power, 2016, 138(4): 042505.
CHILDS D W, VANCE J M.Annular seals as tools to control rotordynamic response of future gas turbine engines [C]//30th Joint Propulsion Conference and Exhibit. Reston, VA, USA: AIAA, 1994: 2804.
KIM N, PARK S Y, RHODE D L.Predicted effects of shunt injection on the rotordynamics of gas labyrinth seals [J]. Journal of Engineering for Gas Turbines and Power, 2003, 125(1): 167-174.
MOORE J J, SOULAS T A.Damper seal comparison in a high-pressure re-injection centrifugal compressor during full-load, full-pressure factory testing using direct rotordynamic stability measurement [C]//ASME 2003 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. New York, NY, USA: ASME, 2003: 1319-1326.
李志刚, 李军, 丰镇平. 进口防旋板对孔型密封非定常气流激振特性的影响 [J]. 西安交通大学学报, 2016, 50(1): 16-21.
LI Zhigang, LI Jun, FENG Zhenping.Effect of swirl brakes on unsteady flow excitation characteristics of hole-pattern seal [J]. Journal of Xi'an Jiaotong University, 2016, 50(1): 16-21.
薛文松, 李志刚, 李军. 防旋板与转子面一体化设计的迷宫密封转子动力特性研究 [J]. 西安交通大学学报, 2022, 56(12): 163-173.
XUE Wensong, LI Zhigang, LI Jun. Rotordynamic characteristics of labyrinth seals with integrated design of swirl brake and shaft configuration [J]. Journal of Xi'an Jiaotong University, 2022, 56(12): 163-173.
IWASAKI M, KAWASHITA R, OMURA N, et al. Effect of partial admission and swirl brakes on destabilization force of labyrinth gas seal [C]///ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. New York, NY, USA: ASME, 2020: V10AT25A003.
NIELSON K K, CHILDS D W, MYLLERUP C M.Experimental and theoretical comparison of two swirl brake designs [J]. Journal of Turbomachinery, 2001, 123(2): 353-358.
WILKES J, SMITH N, VENKATARAMAN B, et al.Experimentally measured effectiveness of different shroud swirl brake profiles in a centrifugal compressor [J]. Journal of Engineering for Gas Turbines and Power, 2023, 145(5): 051012.
CHEN Yaoxing, LI Zhigang, LI Jun, et al. Effects of swirl brake axial arrangement on the leakage performance and rotor stability of labyrinth seals [J]. Chinese Journal of Aeronautics, 2021, 34(1): 22-31.
薛文松, 方志, 王天昊, 等. 防旋板结构的迷宫密封转子动力特性研究 [J]. 西安交通大学学报, 2022, 56(3): 105-116.
XUE Wensong, FANG Zhi, WANG Tianhao, et al.Investigation on the rotordynamic characteristics of labyrinth seal with swirl brakes [J]. Journal of Xi'an Jiaotong University, 2022, 56(3): 105-116.
靳志鸿, 李志刚, 李军, 等. 液氧涡轮泵新型螺旋阻尼密封泄漏特性研究 [J]. 西安交通大学学报, 2022, 56(8): 62-72.
JIN Zhihong, LI Zhigang, LI Jun, et al. Investigation on the leakage characteristics of a novel helical damper seal for the liquid oxygen turbopump [J]. Journal of Xi'an Jiaotong University, 2022, 56(8): 62-72.[23] 靳志鸿, 胡锦华, 李志刚, 等. 液氧涡轮泵阻尼密封设计与动力学特性研究 [J]. 西安交通大学学报, 2023, 57(9): 43-53.
JIN Zhihong, HU Jinhua, LI Zhigang, et al. Investigation on the structural design and rotordynamic characteristics for the damper seal in a liquid oxygen turbopump [J]. Journal of Xi'an Jiaotong University, 2023, 57(9): 43-53.
CHILDS D W.Turbomachinery rotordynamics: phenomena, modeling, and analysis [M]. New York, USA: Wiley, 1993.
LI Zhigang, LI Jun, FENG Zhenping.Numerical comparisons of rotordynamic characteristics for three types of labyrinth gas seals with inlet preswirl [J]. Proceedings of the Institution of Mechanical Engineers: Part A Journal of Power and Energy, 2016, 230(7): 721-738.
0
浏览量
11
下载量
0
CSCD
关联资源
相关文章
相关作者
相关机构
京公网安备11010802024621