Performance Investigation of Stator-Less and Blade-Less Radial ExpanderSource: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 001::page 11014-1Author:Renuke, Avinash
,
Traverso, Alberto
,
Reggio, Federico
,
Pascenti, Matteo
,
Silvestri, Paolo
DOI: 10.1115/1.4063533Publisher: The American Society of Mechanical Engineers (ASME)
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.
|
Show full item record
contributor author | Renuke, Avinash | |
contributor author | Traverso, Alberto | |
contributor author | Reggio, Federico | |
contributor author | Pascenti, Matteo | |
contributor author | Silvestri, Paolo | |
date accessioned | 2024-04-24T22:24:24Z | |
date available | 2024-04-24T22:24:24Z | |
date copyright | 10/26/2023 12:00:00 AM | |
date issued | 2023 | |
identifier issn | 0742-4795 | |
identifier other | gtp_146_01_011014.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4295160 | |
description 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 | The American Society of Mechanical Engineers (ASME) | |
title | Performance Investigation of Stator-Less and Blade-Less Radial Expander | |
type | Journal Paper | |
journal volume | 146 | |
journal issue | 1 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.4063533 | |
journal fristpage | 11014-1 | |
journal lastpage | 11014-14 | |
page | 14 | |
tree | Journal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 001 | |
contenttype | Fulltext |