Technical Papers
Jun 26, 2020

Numerical and Experimental Investigations on Windage Heating Effect of Labyrinth Seals

Publication: Journal of Aerospace Engineering
Volume 33, Issue 5

Abstract

The heat load caused by windage heating effect of labyrinth seals seriously influences the sealing of shaft air flow. To reveal the windage heating effect of labyrinth seals to reasonably design an aeroengine rotor, this paper studies the windage heating characteristics of labyrinth seals from theoretical, numerical, and experimental perspectives. First, the theoretical analysis of the windage heating effect of labyrinth is conducted, and the experimental platform of heating labyrinth was established to test the heating labyrinth effect. Then, an RNGk-ε turbulence model was adopted to investigate the characteristics of flow field, leakage characteristics, and windage heating characteristics of labyrinth seals. Last, the influences of pressure ratio, rotational speed and other factors on the windage heating characteristics of labyrinth seals were investigated by theoretical calculation, numerical simulation, and experiment. Through the comprehensive study, we find that: (1) windage heating is indeed induced when leakage flow absorbs the frictional heat caused by the rub of leakage flow with the rotor; (2) when the speed is lower than 1,000rpm, the windage heating effect is small and enhances with the rise of rotation speed from 1,0006,000  rpm, and the maximum increase of temperature reaches to 12.87 K; and (3) the pressure ratio increases from 11 to 13, and the temperature rise decreases by 7  K. The results of this paper offer a useful insight for the design of labyrinth seals with the emphasis on windage beating effect, to improve the performance of rotor seals.

Get full access to this article

View all available purchase options and get full access to this article.

Data Availability Statement

The data used to support the findings of this study are included within the article.

Acknowledgments

This study is cosupported by the National Natural Science Foundation of China (Grant Nos. 51675351 and 51975124), China’s Postdoctoral Science Funding (Grant No. 2018M633572) and Innovative Talents Support Program of Liaoning Province for the institutions of higher education (Grant No. LR2016033). All authors thank them.

References

Aero Engine Design Manual Editorial Committee. 2002. Aero engine design manual: Transmission and lubrication system. Beijing: Aviation Industry Press.
Chupp, R. E., R. C. Hendricks, S. B. Lattime, and B. M. Steinetz. 2012. “Sealing in turbomachinery.” J. Propul. Power 22 (2): 313–349. https://doi.org/10.2514/1.17778.
Coutier-Delgosha, O., R. Fortes-Patella, and J. L. Reboud. 2008. “Evaluation of the turbulence model influence on the numeric/al simulations of unsteady cavitation.” J. Fluids Eng. 125 (1): 38–45. https://doi.org/10.1115/1.1524584.
Delgado, I. R., and M. P. Proctor. 2006. “Continue investigation of leakage and power loss test results for competing turbine engine seals.” In Proc., 42nd Joint Propulsion Conf. and Exhibit. Sacramento, CA: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2006-4754.
Denecke, J., K. Dullenkopf, S. Wittig, and H. J. Bauer. 2005a. “Experimental investigation of the total temperature increase and swirl development in rotating labyrinth seals.” In Vol. 3 of Proc., ASME Turbo Expo 2005: Power for Land, Sea, and Air, 1161–1171. Reno, NV: International Gas Turbine Institute. https://asmedigitalcollection.asme.org/GT/proceedings-abstract/GT2005/47268/1161/312940.
Denecke, J., J. Färber, K. Dullenkopf, and H. J. Bauer. 2005b. “Dimensional analysis and scaling of rotating seals.” In Vol. 3 of Proc., ASME Turbo Expo 2005: Power for Land, Sea, and Air, 1149–1160. Reno, NV: International Gas Turbine Institute. https://asmedigitalcollection.asme.org/GT/proceedings-abstract/GT2005/47268/1149/312931.
Fei, C. W., G. C. Bai, and W. Z. Tang. 2015. “Probabilistic design of HPT blade-tip radial running clearance with distributed collaborative response surface method.” J. Aerosp. Eng. 28 (2): 04014069. https://doi.org/10.1061/(ASCE)AS.1943-5525.0000399.
Fei, C. W., H. Li, H. T. Liu, C. Lu, and B. Keshtegar. Forthcoming. “Multilevel nested reliability-based design optimization with hybrid intelligent regression for operating assembly relationship.” Aerosp. Sci. Technol. https://doi.org/10.1016/j.ast.2020.105906.
Fei, C. W., C. Lu, and R. P. Liem. 2019. “Decomposed-coordinated surrogate modelling strategy for compound function approximation and a turbine blisk reliability evaluation.” Aerosp. Sci. Technol. 95 (Dec): 105466. https://doi.org/10.1016/j.ast.2019.105466.
Haaser, F., J. Jack, and W. McGreehan. 1988. “Windage rise and flowpath gas ingestions in turbine rim cavities.” J. Eng. Gas Turbines Power 110 (1): 78–85. https://doi.org/10.1115/1.3240090.
Hu, D. Y., J. J. Yang, C. W. Fei, R. Q. Wang, and Y. S. Choy. 2016. “Reliability-based design optimization method of turbine disk with transformed deterministic constraints.” J. Aerosp. Eng. 30 (1): 04016070. https://doi.org/10.1061/(ASCE)AS.1943-5525.0000671.
Kong, X. Z., G. W. Liu, Z. Lei, R. Chang, and Y. Liu. 2016. “Experiment on influence of rotational speeds on labyrinth seals in compressor stator well.” [In Chinese.] J. Aerosp. Power 31 (7): 1575–1582.
Lewis, L. V. 2002. “In-engine measurement of temperature rises in axial, compressor shrouded stator cavities.” In Vol. 3 of Proc., ASME Turbo Expo 2002: Power for Land, Sea, and Air, 781–794. Amsterdam, Netherlands: International Gas Turbine Institute. https://asmedigitalcollection.asme.org/GT/proceedings-abstract/GT2002/36088/781/296286.
Lu, C., Y. W. Feng, C. W. Fei, and S. Q. Bu. 2019. “Improved decomposed-coordinated kriging modeling strategy for dynamic probabilistic analysis of multi-component structures.” IEEE Trans. Reliab. 69 (2): 440–457. https://doi.org/10.1109/TR.2019.2954379.
Luo, X., D. Zang, Z. Tao, G. Xu, and Q. Wang. 2014. “Windage measurements in a rotor-stator system with superimposed cooling and rotor-mounted protrusions.” J. Eng. Gas Turbines Power 136 (4): 042505. https://doi.org/10.1115/1.4026086.
McGreehan, W. F., and S. H. Ko. 1989. “Power dissipation in smooth and honeycomb labyrinth seals.” In Vol. 1 of Proc., ASME 1989 Int. Gas Turbine and Aeroengine Congress and Exposition: Turbomachinery. Toronto: International Gas Turbine Institute. https://asmedigitalcollection.asme.org/GT/proceedings/GT1989/79139/V001T01A088/239861.
Millward, J., and M. Edwards. 1996. “Windage heating of air passing through labyrinth seals.” J. Turbomach. 118 (2): 414–419. https://doi.org/10.1115/1.2836657.
Nayak, K., M. Mohamed, and A. Ansari. 2007. “The effects of tooth tip wear and its axial displacement in rub-grooves on leakage and windage heating of labyrinth seals with honeycomb lands.” In Proc., 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conf. and Exhibit, 5736. Cincinnati: American Institute of Aeronautics and Astronautics. https://doi.org/10.2514/6.2007-5736.
Nayak, K. C., and P. Dutta. 2016. “Numerical investigations for leakage and windage heating in straight-through labyrinth seals.” J. Eng. Gas Turbines Power 138 (1): 012507. https://doi.org/10.1115/1.4031343.
Scherer, T., W. Waschka, and S. Wittig. 1992. “Numerical predictions of high speed rotating labyrinth seals performance: Influence of rotation on power dissipation and temperature rise.” In Proc., ICHMT Int. Symp. on Heat Transfer in Turbomachinery, 233–244. Athens, Greece: International Centre for Heat and Mass Transfer. https://www.dl.begellhouse.com/references/1bb331655c289a0a,1ab192ea462ccfaf,040dcd954a2cb369.html.
Steinetz, B. M., R. C. Hendricks, and J. Munson. 1998. Advanced seal technology role in meeting next generation turbine engine goals. Cleveland: National Aeronautics and Space Administration, Lewis Research Center.
Stocker, H. L., D. M. Cox, and G. F. Holle. 1997. Aerodynamic performance of conventional and advanced design labyrinth seals with solid-smooth, abradable and honeycomb lands. Washington, DC: National Aeronautics and Space Administration.
Tao, Z., D. Zhang, X. Luo, G. Xu, and J. Han. 2014. “Windage heating in a shrouded rotor-stator system.” J. Eng. Gas Turbines Power 136 (6): 062602. https://doi.org/10.1115/1.4026429.
Yan, X., J. Li, L. Song, and Z. Feng. 2009. “Investigations on the discharge and total temperature increase characteristics of the labyrinth seals with honeycomb and smooth lands.” J. Turbomach. 131 (4): 041009. https://doi.org/10.1115/1.3068320.

Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 33Issue 5September 2020

History

Received: Dec 30, 2019
Accepted: Apr 23, 2020
Published online: Jun 26, 2020
Published in print: Sep 1, 2020
Discussion open until: Nov 26, 2020

Permissions

Request permissions for this article.

Authors

Affiliations

Professor, Liaoning Key Lab of Advanced Test Technology for Aerospace Propulsion System, Shenyang Aerospace Univ., Shenyang 110136, PR China. Email: [email protected]
Liaoning Key Lab of Advanced Test Technology for Aerospace Propulsion System, Shenyang Aerospace Univ., Shenyang 110136, PR China. Email: [email protected]
Professor, Liaoning Key Lab of Advanced Test Technology for Aerospace Propulsion System, Shenyang Aerospace Univ., Shenyang 110136, PR China. Email: [email protected]
Liaoning Key Lab of Advanced Test Technology for Aerospace Propulsion System, Shenyang Aerospace Univ., Shenyang 110136, PR China. Email: [email protected]
Professor, Dept. of Aeronautics and Astronautics, Fudan Univ., Shanghai 200433, PR China (corresponding author). ORCID: https://orcid.org/0000-0001-5333-1055. Email: [email protected]
M.Sc. Student, Dept. of Aeronautics and Astronautics, Fudan Univ., Shanghai 200433, PR China. Email: [email protected]

Metrics & Citations

Metrics

Citations

Download citation

If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.

Cited by

View Options

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Media

Figures

Other

Tables

Share

Share

Copy the content Link

Share with email

Email a colleague

Share