Performance Investigation of Stator-Less and Blade-Less Radial Expander

Author:

Renuke Avinash1,Traverso Alberto2,Reggio Federico3,Pascenti Matteo4,Silvestri Paolo3

Affiliation:

1. Malardalen University, Vasteras 72123, Sweden

2. University of Genoa, TPG, Genoa 16145, Italy

3. University of Genoa, Genoa 16145, Italy

4. SIT Technologies srl, Genoa 16145, Italy

Abstract

Abstract Interests in small-scale turbomachinery are gaining momentum, particularly around waste heat recovery using Organic Rankine Cycle (ORC), energy harvesting, pico-hydro, refrigeration and heat pumps and small-scale power generation. These applications demand to have economical, simple construction, and reasonably efficient machines. The performance of bladed turbomachine at a small scale is poor mainly due to viscous losses and relatively large clearances. In some cases, like ORC, it requires a lubrication system, making it complex and costly. Bladeless or Tesla turbomachinery is seen as one of the solutions for these applications due to its simple construction and cost-effectiveness. However, the experimental efficiency of the bladeless turbines/compressors is found in the low region, <40%. In this article, the performance of a bladeless turbine is investigated using a vaneless volute configuration, making the turbine stator-less (vaneless volute) and bladeless (vaneless rotor). This study presents numerical and experimental performance investigation with a volute as a stator of the bladeless rotor. Three-dimensional (3D) Numerical results show very promising performance of the turbine with total to static efficiencies calculated above 65%. In the second part of the article, turbine prototype components, assembly, and test setup are discussed. Experimental maximum efficiency of 41.5 ± 0.88% at 3.5 kg/s@5000 rpm and power of 915 W is obtained. This is the highest recorded efficiency for the Tesla turbine in peer-reviewed research. The overall turbine performance from 3D numerical simulation with ventilation and mechanical losses is compared with experimental results. This work demonstrates that the proposed stator-less/volute configuration provides an efficient way for bladeless or Tesla turbines, particularly for low-head applications.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference24 articles.

1. Turbine,1913

2. Fluid Propulsion,1913

3. Experimental Characterization of Losses in Bladeless Turbine Prototype;ASME J. Eng. Gas Turbines Power,2022

4. Reverse Cycle Machine Provided With a Turbine,2018

5. Armstrong, J. H., 1952, “ An Investigation of the Performance of a Modified Tesla Turbine,” Ph.D. thesis, Faculty of the Division of Graduate Studies, Georgia Institute of Technology, Atlanta, GA.http://hdl.handle.net/1853/19556

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