LAPSE:2023.4721
Published Article

LAPSE:2023.4721
Optimizing the Geometric Parameters of a Stepped Labyrinth Seal to Minimize the Discharge Coefficient
February 23, 2023
Abstract
A series of numerical simulations were performed to study the discharge coefficient based on the geometric parameters of a stepped labyrinth seal that sealed the secondary flow path of a gas turbine. In contrast with straight-through seals, stepped labyrinth seals introduce additional geometrical parameters related to the steps. In this study, three shape variables were observed: step height (SH), position, and cavity width (CW). The sensitivity to the leakage flow of the shape variable in the stepped labyrinth seal was analyzed. The mechanism for improving the sealing performance of stepped labyrinth seals was investigated. The results indicated that the stepped labyrinth seal exhibited up to 17.9% higher leakage-suppression performance than the straight labyrinth seal. Seals with large discharge coefficients had a large vena contracta upstream of each tooth structure and a rapidly accelerated axial velocity in the radial direction. We could observe that the discharge coefficient changed according to the flow field in the cavity. The wall shear stress was sensitive to the SH but not to the CW or step position.
A series of numerical simulations were performed to study the discharge coefficient based on the geometric parameters of a stepped labyrinth seal that sealed the secondary flow path of a gas turbine. In contrast with straight-through seals, stepped labyrinth seals introduce additional geometrical parameters related to the steps. In this study, three shape variables were observed: step height (SH), position, and cavity width (CW). The sensitivity to the leakage flow of the shape variable in the stepped labyrinth seal was analyzed. The mechanism for improving the sealing performance of stepped labyrinth seals was investigated. The results indicated that the stepped labyrinth seal exhibited up to 17.9% higher leakage-suppression performance than the straight labyrinth seal. Seals with large discharge coefficients had a large vena contracta upstream of each tooth structure and a rapidly accelerated axial velocity in the radial direction. We could observe that the discharge coefficient changed according to the flow field in the cavity. The wall shear stress was sensitive to the SH but not to the CW or step position.
Record ID
Keywords
discharge coefficient, gas turbine, labyrinth seal, Reynolds-averaged Navier–Stokes (RANS), vena contracta
Subject
Suggested Citation
Chun YH, Ahn J. Optimizing the Geometric Parameters of a Stepped Labyrinth Seal to Minimize the Discharge Coefficient. (2023). LAPSE:2023.4721
Author Affiliations
Chun YH: Department of Mechanical Engineering, Graduate School, Kookmin University, 77 Jeongneung-ro, Seongbuk-gu, Seoul 02707, Korea
Ahn J: School of Mechanical Engineering, Kookmin University, Seoul 02707, Korea [ORCID]
Ahn J: School of Mechanical Engineering, Kookmin University, Seoul 02707, Korea [ORCID]
Journal Name
Processes
Volume
10
Issue
10
First Page
2019
Year
2022
Publication Date
2022-10-06
ISSN
2227-9717
Version Comments
Original Submission
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PII: pr10102019, Publication Type: Journal Article
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LAPSE:2023.4721
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https://doi.org/10.3390/pr10102019
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[v1] (Original Submission)
Feb 23, 2023
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Feb 23, 2023
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