Abstract
This paper presents a study conducted on a new gas turbine designed to limit leakage in the labyrinth seal. The slots in the fin are used to generate a bypass flow, which obstructs the flow in the gap above the fin. The method was tested numerically and experimentally beforehand using a simplified model without rotation or blade passages. In this paper, the validation of the method using a model of a turbine stage is shown. Reynolds-averaged Navier–Stokes simulations using two turbulence models—Spalart–Allmaras (SA) and k-ω EARSM—were conducted. Comparisons of leakage flow and stage efficiency for reference and fluidic sealing configurations are presented. Fluidic sealing configuration is effective and reduces the leakage flow by 13–18.5% (depending on the turbulence model). The analysis of the flow structure in the seal region revealed that the use of fluidic sealing resulted in significant circumferential flow anisotropy.
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- Accepted or Published Version
- DOI:
- Digital Object Identifier (open in new tab) 10.1115/1.4064045
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- Category:
- Articles
- Type:
- artykuły w czasopismach
- Published in:
-
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME
no. 146,
ISSN: 0889-504X - Language:
- English
- Publication year:
- 2024
- Bibliographic description:
- Wasilczuk F., Flaszyński P., Doerffer P., Marugi K., Borzęcki T.: The Application of Fluidic Sealing in Shrouded Gas Turbine Blades// JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME -Vol. 146,iss. 1 (2024),
- DOI:
- Digital Object Identifier (open in new tab) 10.1115/1.4064045
- Sources of funding:
-
- Free publication
- Verified by:
- Gdańsk University of Technology
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