Implications of Phase Change on the Aerodynamics of Centrifugal Compressors for Supercritical Carbon Dioxide ApplicationsSource: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 004::page 041007-1Author:Persico, Giacomo
,
Gaetani, Paolo
,
Romei, Alessandro
,
Toni, Lorenzo
,
Bellobuono, Ernani Fulvio
,
Valente, Roberto
DOI: 10.1115/1.4049924Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Closed Joule–Brayton cycles operating with carbon dioxide in supercritical conditions (sCO2) are nowadays collecting a significant scientific interest, due to their high potential efficiency, the compactness of their components, and the flexibility that makes them suitable to exploit diverse energy sources. However, the technical implementation of sCO2 power systems introduces new challenges related to the design and operation of the components. The compressor, in particular, operates in a thermodynamic condition close to the critical point, whereby the fluid exhibits significant non-ideal gas effects and is prone to phase change in the intake region of the machine. These new challenges require novel design concepts and strategies, as well as proper tools to achieve reliable predictions. In this study, we consider an exemplary sCO2 power cycle with the main compressor operating in proximity to the critical point, with an intake entropy level of the fluid lower than the critical value. In this condition, the phase change occurs as evaporation/flashing, thus resembling cavitation phenomena observed in liquid pumps, even though with specific issues associated with compressibility effects occurring in both the phases. The flow configuration is therefore highly nonconventional and demands the development of proper tools for fluid and flow modeling, which are instrumental for the compressor design. The paper discusses the modeling issues from the thermodynamic perspective, then highlighting their implications on compressor aerodynamics. We propose tailored models to account for the effect of the phase change in 0D mean-line design tools as well as in fully three-dimensional (3D) computational fluid-dynamic (CFD) simulations: the former was previously validated for sCO2 compressors, the latter is validated in this paper against experiments of compressible flows of supercritical sCO2 in nozzles. In this way, a strategy of investigation is built-up as a combination of mean-line tools, industrial design experience, and CFD for detailed flow analysis. The investigation reveals that the potential onset of the phase change might alter significantly the performance and operation of the compressor, both in design and in off-design conditions, according to three main mechanisms: incidence effect, front-loading, and channel blockage.
|
Show full item record
contributor author | Persico, Giacomo | |
contributor author | Gaetani, Paolo | |
contributor author | Romei, Alessandro | |
contributor author | Toni, Lorenzo | |
contributor author | Bellobuono, Ernani Fulvio | |
contributor author | Valente, Roberto | |
date accessioned | 2022-02-05T22:20:32Z | |
date available | 2022-02-05T22:20:32Z | |
date copyright | 2/24/2021 12:00:00 AM | |
date issued | 2021 | |
identifier issn | 0742-4795 | |
identifier other | gtp_143_04_041007.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4277367 | |
description abstract | Closed Joule–Brayton cycles operating with carbon dioxide in supercritical conditions (sCO2) are nowadays collecting a significant scientific interest, due to their high potential efficiency, the compactness of their components, and the flexibility that makes them suitable to exploit diverse energy sources. However, the technical implementation of sCO2 power systems introduces new challenges related to the design and operation of the components. The compressor, in particular, operates in a thermodynamic condition close to the critical point, whereby the fluid exhibits significant non-ideal gas effects and is prone to phase change in the intake region of the machine. These new challenges require novel design concepts and strategies, as well as proper tools to achieve reliable predictions. In this study, we consider an exemplary sCO2 power cycle with the main compressor operating in proximity to the critical point, with an intake entropy level of the fluid lower than the critical value. In this condition, the phase change occurs as evaporation/flashing, thus resembling cavitation phenomena observed in liquid pumps, even though with specific issues associated with compressibility effects occurring in both the phases. The flow configuration is therefore highly nonconventional and demands the development of proper tools for fluid and flow modeling, which are instrumental for the compressor design. The paper discusses the modeling issues from the thermodynamic perspective, then highlighting their implications on compressor aerodynamics. We propose tailored models to account for the effect of the phase change in 0D mean-line design tools as well as in fully three-dimensional (3D) computational fluid-dynamic (CFD) simulations: the former was previously validated for sCO2 compressors, the latter is validated in this paper against experiments of compressible flows of supercritical sCO2 in nozzles. In this way, a strategy of investigation is built-up as a combination of mean-line tools, industrial design experience, and CFD for detailed flow analysis. The investigation reveals that the potential onset of the phase change might alter significantly the performance and operation of the compressor, both in design and in off-design conditions, according to three main mechanisms: incidence effect, front-loading, and channel blockage. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Implications of Phase Change on the Aerodynamics of Centrifugal Compressors for Supercritical Carbon Dioxide Applications | |
type | Journal Paper | |
journal volume | 143 | |
journal issue | 4 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.4049924 | |
journal fristpage | 041007-1 | |
journal lastpage | 041007-11 | |
page | 11 | |
tree | Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 004 | |
contenttype | Fulltext |