A Comparison of the Flow Structures and Losses Within Vaned and Vaneless Stators for Radial Turbines

Author:

Simpson A. T.1,Spence S. W. T.1,Watterson J. K.1

Affiliation:

1. School of Mechanical & Aerospace Engineering, Queen’s University Belfast, Ashby Building, Stranmillis Road, Belfast BT9 5AH, UK

Abstract

This paper details the numerical analysis of different vaned and vaneless radial inflow turbine stators. Selected results are presented from a test program carried out to determine performance differences between the radial turbines with vaned stators and vaneless volutes under the same operating conditions. A commercial computational fluid dynamics code was used to develop numerical models of each of the turbine configurations, which were validated using the experimental results. From the numerical models, areas of loss generation in the different stators were identified and compared, and the stator losses were quantified. Predictions showed the vaneless turbine stators to incur lower losses than the corresponding vaned stator at matching operating conditions, in line with the trends in measured performance. Flow conditions at rotor inlet were studied and validated with internal static pressure measurements so as to judge the levels of circumferential nonuniformity for each stator design. In each case, the vaneless volutes were found to deliver a higher level of uniformity in the rotor inlet pressure field.

Publisher

ASME International

Subject

Mechanical Engineering

Reference17 articles.

1. Investigation of Flow in the Nozzle-Less Spiral Casing of a Radial Inward-Flow Gas Turbine;Bhinder;Proc. Inst. Mech. Eng.

2. Palmer, R. M. , 1955, “D.I.G.T. Radial Inflow Turbine—Scroll and Nozzle Performance—Part I,” Ricardo Internal Report No. 1365A.

3. Palmer, R. M. , 1955, “D.I.G.T. Radial Inflow Turbine—Scroll and Nozzle Performance—Part II,” Ricardo Internal Report No. 1368.

4. Flows in Vaned and Vaneless Stators of Radial Inflow Turbocharger Turbines;Baines

5. Laser Velocimeter Measurements at the Rotor Inlet of a Turbocharger Radial Inflow Turbine;Benisek

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