Numerical analysis on leakage flow of blade tip stepped seal in steam turbine

被引:1
|
作者
Cao L.-H. [1 ]
Jia Y.-M. [1 ]
Li P. [1 ]
Hu P.-F. [1 ]
Li Y. [1 ]
机构
[1] School of Energy and Power Engineering, Northeast Dianli University, Jilin, 132012, Jilin Province
关键词
Blade tip seal; Entropy production; Leakage flow; Steam turbine; Three-dimensional streamlines;
D O I
10.3785/j.issn.1008-973X.2016.08.017
中图分类号
学科分类号
摘要
The three-dimensional steady numerical simulation was performed to study the influence of the tip clearances and the teeth number on the blade tip leakage flow rate, the three-dimensional streamlines in the seal and at the exit of rotor blade, and the distribution of entropy production at the exit of rotor blade, by taking the first high-pressure stage of a steam turbine with the blade tip stepped seal as object. Results indicate that the increase of tip clearance cause the increase of the leakage flow rate, the skewing of three-dimensional streamlines at the exit of rotor blade, the region of entropy production and the mixing loss. The increase of teeth number of tip stepped seal cause the decrease of the leakage flow rate, the skewing of three-dimensional streamlines at the exit of rotor blade, the entropy production and the mixing loss. The mixing loss caused by blade tip leakage flow is mainly on the 7% region of the top exit of rotor blade. © 2016, Zhejiang University Press. All right reserved.
引用
收藏
页码:1545 / 1550
页数:5
相关论文
共 15 条
  • [1] Matsunuma T., Unsteady flow field of an Axial-flow turbine rotor at a low Reynolds number, ASME Journal of Turbomachinery, 129, 2, pp. 360-371, (2007)
  • [2] Cecco D.S., Yaras M.I., Sjolander S.A., Measurement of tip leakage flows in turbine cascade with large clearances, Proceedings of the International Gas Turbine and Aeroengine Congress and Exposition, pp. 1-12, (1995)
  • [3] Deng Q.-F., Zheng Q., Zhang H., Et al., Analysis of secondary flow vortex structure and losses in a high load turbine designed by the controlled vortex method, Proceedings of the CSEE, 32, 20, pp. 108-114, (2012)
  • [4] Li P., Zhang D., He L., Et al., Study on three dimensional flow of last stage with lashing wire and tip clearance in steam turbine, Proceedings of the CSEE, 31, 8, pp. 80-86, (2011)
  • [5] Yoon S., Curtis E., Denton J., Et al., The effect of clearance on shrouded and unshrouded turbines at two levels of reaction, ASME Journal of Turbomachinery, 136, 2, pp. 1231-1241, (2010)
  • [6] Gier J., Stubert B., Interaction of shroud leakage flow and main flow in a three-stage LP turbine, ASME Journal of Turbomachinery, 127, 4, pp. 649-658, (2005)
  • [7] Rosic B., Denton J.D., Curtis E.M., The influence of shroud and cavity geometry on turbine performance: an experimental and computational study: Part I: shroud geometry, ASME Journal of Turbomachinery, 130, (2008)
  • [8] Porreca L., Behr T., Schlienger J., Et al., Fluid dynamics and performance of partially and fully shrouded axial turbines, ASME Journal of Turbomachinery, 127, 4, pp. 668-678, (2005)
  • [9] Bindon J.P., The Measurement and formation of tip clearance loss, ASME Journal of Turbomachinery, 111, 3, pp. 257-263, (1989)
  • [10] Liu Y., Liu P.-N., Jiang W.-H., Et al., Experiment on clearance leakage flow and aerodynamic performence in shrouded turbine cascade, Journal of Aerospace Power, 28, 10, pp. 2291-2301, (2013)