Influence of tip-gap losses on the stage efficiency of downsizing turbocharger turbines

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Autoren

  • J. Kammeyer
  • C. Natkaniec
  • J. R. Seume
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Details

OriginalspracheEnglisch
Titel des Sammelwerks9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group
Seiten293-306
Seitenumfang14
PublikationsstatusVeröffentlicht - 2010
Veranstaltung9th International Conference on Turbochargers and Turbocharging - Westminster, London, Großbritannien / Vereinigtes Königreich
Dauer: 19 Mai 201020 Mai 2010

Publikationsreihe

Name9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group

Abstract

Experimental investigations on a turbocharger test stand and numerical simulations with CFD were carried out to better understand the loss mechanisms in turbocharger turbines for engine downsizing applications. This paper describes the tip-leakage flow mechanisms in small turbocharger turbines and the influences of the tip-gap losses on the turbine stage efficiency. In addition to the common mechanisms of scraping and tip-leakage, the so called "axial blow-by" is identified as another result of tip-leakage. It was found that the relative tip-leakage losses in small radial turbines increase only slightly with decreasing dimensions, while the total leakage losses show a severe and disproportional increase. Empirical correlations are suggested to estimate the tip-gap losses of radial turbines in preliminary design of turbochargers or engine applications.

ASJC Scopus Sachgebiete

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Influence of tip-gap losses on the stage efficiency of downsizing turbocharger turbines. / Kammeyer, J.; Natkaniec, C.; Seume, J. R.
9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group. 2010. S. 293-306 (9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group).

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Kammeyer, J, Natkaniec, C & Seume, JR 2010, Influence of tip-gap losses on the stage efficiency of downsizing turbocharger turbines. in 9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group. 9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group, S. 293-306, 9th International Conference on Turbochargers and Turbocharging, Westminster, London, Großbritannien / Vereinigtes Königreich, 19 Mai 2010. https://doi.org/10.1243/17547164C0012010023
Kammeyer, J., Natkaniec, C., & Seume, J. R. (2010). Influence of tip-gap losses on the stage efficiency of downsizing turbocharger turbines. In 9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group (S. 293-306). (9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group). https://doi.org/10.1243/17547164C0012010023
Kammeyer J, Natkaniec C, Seume JR. Influence of tip-gap losses on the stage efficiency of downsizing turbocharger turbines. in 9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group. 2010. S. 293-306. (9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group). doi: 10.1243/17547164C0012010023
Kammeyer, J. ; Natkaniec, C. ; Seume, J. R. / Influence of tip-gap losses on the stage efficiency of downsizing turbocharger turbines. 9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group. 2010. S. 293-306 (9th International Conference on Turbochargers and Turbocharging - Institution of Mechanical Engineers, Combustion Engines and Fuels Group).
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abstract = "Experimental investigations on a turbocharger test stand and numerical simulations with CFD were carried out to better understand the loss mechanisms in turbocharger turbines for engine downsizing applications. This paper describes the tip-leakage flow mechanisms in small turbocharger turbines and the influences of the tip-gap losses on the turbine stage efficiency. In addition to the common mechanisms of scraping and tip-leakage, the so called {"}axial blow-by{"} is identified as another result of tip-leakage. It was found that the relative tip-leakage losses in small radial turbines increase only slightly with decreasing dimensions, while the total leakage losses show a severe and disproportional increase. Empirical correlations are suggested to estimate the tip-gap losses of radial turbines in preliminary design of turbochargers or engine applications.",
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