Supersonic impulse turbine for automotive waste heat recovery: A comparison of three designs of turbine blade profiles

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

Autorschaft

  • Harald S. Kunte
  • Joerg R. Seume
  • Dmitrii V. Pautov
  • Marina G. Cherkasova
  • Nicholay A. Zabelin
  • Sergey Y. Olennikov
  • Victor A. Rassokhin

Externe Organisationen

  • St. Petersburg State Polytechnical University
Forschungs-netzwerk anzeigen

Details

OriginalspracheEnglisch
Titel des Sammelwerks11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2015
PublikationsstatusVeröffentlicht - 2015
Veranstaltung11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2015 - Madrid, Spanien
Dauer: 23 März 201527 März 2015

Abstract

One current approach considered by automobile manufacturers to recover waste heat uses Organic Rankine Cycles (ORC) to increase the efficiency of combustion engines. However the efficiency of these ORCs is strongly dependent on the efficiency of a suitable expansion machine. For a suitable choice, three different turbines are compared, which are designed for a predefined operating point of such an automobile ORC. These turbines are partially admitted impulse turbines with a trapezoidal Laval nozzle, a circular Laval nozzle and a trapezoidal Laval nozzle with a small expansion ratio in the divergent nozzle part. The scope of this comparison is the performance of the turbines at full and partial admission. To this end, the full admission turbines are numerically investigated with CFD and the losses due to partial admission are considered by an empirical approach. Finally, the losses due to partial admission are shown separately and their main sensitivities are identified.

ASJC Scopus Sachgebiete

Zitieren

Supersonic impulse turbine for automotive waste heat recovery: A comparison of three designs of turbine blade profiles. / Kunte, Harald S.; Seume, Joerg R.; Pautov, Dmitrii V. et al.
11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2015. 2015.

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

Kunte, HS, Seume, JR, Pautov, DV, Cherkasova, MG, Zabelin, NA, Olennikov, SY & Rassokhin, VA 2015, Supersonic impulse turbine for automotive waste heat recovery: A comparison of three designs of turbine blade profiles. in 11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2015. 11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2015, Madrid, Spanien, 23 März 2015.
Kunte, H. S., Seume, J. R., Pautov, D. V., Cherkasova, M. G., Zabelin, N. A., Olennikov, S. Y., & Rassokhin, V. A. (2015). Supersonic impulse turbine for automotive waste heat recovery: A comparison of three designs of turbine blade profiles. In 11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2015
Kunte HS, Seume JR, Pautov DV, Cherkasova MG, Zabelin NA, Olennikov SY et al. Supersonic impulse turbine for automotive waste heat recovery: A comparison of three designs of turbine blade profiles. in 11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2015. 2015
Kunte, Harald S. ; Seume, Joerg R. ; Pautov, Dmitrii V. et al. / Supersonic impulse turbine for automotive waste heat recovery : A comparison of three designs of turbine blade profiles. 11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2015. 2015.
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abstract = "One current approach considered by automobile manufacturers to recover waste heat uses Organic Rankine Cycles (ORC) to increase the efficiency of combustion engines. However the efficiency of these ORCs is strongly dependent on the efficiency of a suitable expansion machine. For a suitable choice, three different turbines are compared, which are designed for a predefined operating point of such an automobile ORC. These turbines are partially admitted impulse turbines with a trapezoidal Laval nozzle, a circular Laval nozzle and a trapezoidal Laval nozzle with a small expansion ratio in the divergent nozzle part. The scope of this comparison is the performance of the turbines at full and partial admission. To this end, the full admission turbines are numerically investigated with CFD and the losses due to partial admission are considered by an empirical approach. Finally, the losses due to partial admission are shown separately and their main sensitivities are identified.",
author = "Kunte, {Harald S.} and Seume, {Joerg R.} and Pautov, {Dmitrii V.} and Cherkasova, {Marina G.} and Zabelin, {Nicholay A.} and Olennikov, {Sergey Y.} and Rassokhin, {Victor A.}",
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Download

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T2 - 11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC 2015

AU - Kunte, Harald S.

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AU - Zabelin, Nicholay A.

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