Analysis of gas turbine rim cavity ingestion with axial purge flow injection

Christopher W. Robak, Amir Faghri, Karen A. Thole

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

Turbine rim cavities require an adequate supply of cooling purge flow to prevent hot gas ingestion from overheating metal components beneath the gas path airfoils. Purge flow is typically introduced into rim cavities through a labyrinth seal at the inner diameter of the cavity, or through conduits in the metal walls of the rim cavity. This numerical study will focus on purge flow introduced through axial holes in the stationary side of a turbine realistic rim cavity. Three dimensional Unsteady Reynolds-average Navier-Stokes (URANS) CFD modeling is utilized to model of cavity sealing effectiveness as a function of axial purge flow rate. CFD modeling is compared with experimental data from the test turbine in the Steady Thermal Aero Research Turbine (START). Results show good agreement with experimental data, especially at lower purge flow rates. Analytical depictions of the flow field setup in the rim cavity are provided, explaining trends observed in experimental data. Differences in sealing effectiveness trends between the upper and lower portions of the rim cavity are predicted by CFD modeling, adding insight to ingestion phenomena in turbine realistic rim cavities with complex geometry and flow leakage paths.

Original languageEnglish (US)
Title of host publicationHeat Transfer
PublisherAmerican Society of Mechanical Engineers (ASME)
ISBN (Electronic)9780791858653
DOIs
StatePublished - Jan 1 2019
EventASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019 - Phoenix, United States
Duration: Jun 17 2019Jun 21 2019

Publication series

NameProceedings of the ASME Turbo Expo
Volume5B-2019

Conference

ConferenceASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019
CountryUnited States
CityPhoenix
Period6/17/196/21/19

Fingerprint

Axial flow
Gas turbines
Turbines
Computational fluid dynamics
Flow rate
Metals
Gases
Airfoils
Seals
Flow fields
Cooling
Geometry

All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Robak, C. W., Faghri, A., & Thole, K. A. (2019). Analysis of gas turbine rim cavity ingestion with axial purge flow injection. In Heat Transfer (Proceedings of the ASME Turbo Expo; Vol. 5B-2019). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/GT2019-91807
Robak, Christopher W. ; Faghri, Amir ; Thole, Karen A. / Analysis of gas turbine rim cavity ingestion with axial purge flow injection. Heat Transfer. American Society of Mechanical Engineers (ASME), 2019. (Proceedings of the ASME Turbo Expo).
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Robak, CW, Faghri, A & Thole, KA 2019, Analysis of gas turbine rim cavity ingestion with axial purge flow injection. in Heat Transfer. Proceedings of the ASME Turbo Expo, vol. 5B-2019, American Society of Mechanical Engineers (ASME), ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition, GT 2019, Phoenix, United States, 6/17/19. https://doi.org/10.1115/GT2019-91807

Analysis of gas turbine rim cavity ingestion with axial purge flow injection. / Robak, Christopher W.; Faghri, Amir; Thole, Karen A.

Heat Transfer. American Society of Mechanical Engineers (ASME), 2019. (Proceedings of the ASME Turbo Expo; Vol. 5B-2019).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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Robak CW, Faghri A, Thole KA. Analysis of gas turbine rim cavity ingestion with axial purge flow injection. In Heat Transfer. American Society of Mechanical Engineers (ASME). 2019. (Proceedings of the ASME Turbo Expo). https://doi.org/10.1115/GT2019-91807