Effect of volute geometry on the steady and unsteady performance of mixed-flow turbines

Author:

Hakeem I1,Su C-C2,Costall A3,Martinez-Botas R. F.3

Affiliation:

1. Mechanical Engineering Department, Institute Technology Brunei, Negara Brunei Darussalam

2. Mechanical Engineering Department, Yung-Ta Institute of Technology and Commerce, Ping-Tung, Taiwan

3. Mechanical Engineering Department, Imperial College London, London, England

Abstract

The steady and unsteady performance of two mixed-flow turbocharger turbine rotors has been investigated. These rotors differ mainly in their inlet blade angle geometry; one has a constant blade angle (rotor A) and the other a notionally constant incidence angle (rotor B). The results indicate that the constant blade inlet angle design offers improved efficiency characteristics over the constant incidence one with total-to-static efficiency at the design point ranging between 0.7 and 0.76. A detailed assessment of the influence of volute geometry on the turbine performance has been carried out, which confirmed that the geometry of volute plays a critical role in the overall performance of a turbine. The unsteady performance tests have indicated a substantial deviation from the performance and flow characteristics of equivalent steady-state tests, which is quantified and discussed.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Energy Engineering and Power Technology

Reference15 articles.

1. Design of a Highly Loaded Mixed Flow Turbine

2. Baines N. C., Lavy M. Flows in vaned and vaneless stators of radial-inflow turbocharger turbines. In Proceedings of IMechE International Conference on Turbochargers and turbocharging, 1990, pp. 7–12 (Mechanical Engineering Publications, London).

3. Naguib M. Experience with the modern RR151 turbocharger for high-speed diesel engines. IMechE Conference on Turbocharging and turbochargers, London, 1986, pp. 105–112 (Mechanical Engineering Publications, London).

4. Analytical Optimization Design of Radial and Mixed Flow Turbines

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