Three-dimensional Reynolds-averaged Navier–Stokes solutions are employed to investigate the discharge and total temperature increase characteristics of the stepped labyrinth seal with honeycomb land. First, the relations between the windage heating number and the circumferential Mach number at different Reynolds numbers for different honeycomb seals are calculated and compared with the experimental data. The obtained numerical results show that the present three-dimensional periodic model can properly predict the total temperature increase in honeycomb seals. Then, a range of pressure ratios, three inlet preswirl ratios, four sizes of honeycomb cell diameter, and nine sizes of cell depth are selected to investigate the influence of inlet preswirl ratios and honeycomb geometry sizes on the discharge and total temperature increase characteristics of the stepped labyrinth seal. It shows that the leakage rate increases with the increase in cell diameter, and the cell depth has a strong influence on the discharge behavior. However, the influence of the inlet preswirl on the leakage rate is found to be little in the present study. For the total temperature increase characteristic, the inlet preswirl ratio and pressure ratio have more pronounced influence than those of cell depth and diameter. Furthermore, the relations between the leakage rate and cell depth and diameter, as well as the relations between the windage heating power and cell depth and diameter, are not monotonic functions if the pressure ratio is kept constant.
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December 2010
Research Papers
Effects of Inlet Preswirl and Cell Diameter and Depth on Honeycomb Seal Characteristics
Xin Yan,
Xin Yan
Institute of Turbomachinery, School of Energy and Power Engineering,
Xi’an Jiaotong University
, Xi’an 710049, P.R.China
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Jun Li,
Jun Li
Institute of Turbomachinery, School of Energy and Power Engineering,
e-mail: junli@mail.xjtu.edu.cn
Xi’an Jiaotong University
, Xi’an 710049, P.R.China
Search for other works by this author on:
Zhenping Feng
Zhenping Feng
Institute of Turbomachinery, School of Energy and Power Engineering,
Xi’an Jiaotong University
, Xi’an 710049, P.R.China
Search for other works by this author on:
Xin Yan
Institute of Turbomachinery, School of Energy and Power Engineering,
Xi’an Jiaotong University
, Xi’an 710049, P.R.China
Jun Li
Institute of Turbomachinery, School of Energy and Power Engineering,
Xi’an Jiaotong University
, Xi’an 710049, P.R.Chinae-mail: junli@mail.xjtu.edu.cn
Zhenping Feng
Institute of Turbomachinery, School of Energy and Power Engineering,
Xi’an Jiaotong University
, Xi’an 710049, P.R.ChinaJ. Eng. Gas Turbines Power. Dec 2010, 132(12): 122506 (13 pages)
Published Online: August 30, 2010
Article history
Received:
October 8, 2009
Revised:
January 11, 2010
Online:
August 30, 2010
Published:
August 30, 2010
Citation
Yan, X., Li, J., and Feng, Z. (August 30, 2010). "Effects of Inlet Preswirl and Cell Diameter and Depth on Honeycomb Seal Characteristics." ASME. J. Eng. Gas Turbines Power. December 2010; 132(12): 122506. https://doi.org/10.1115/1.4001296
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