Performance Analysis of Transcritical Carbon Dioxide Rankine Cycle with Regenerator

Transcritical carbon dioxide Rankine cycle (TCRC) has a potential to convert low grade heat source into power. Thus, the objective of this paper is to evaluate TCRC performance based on the first and the second law of thermodynamics for wide and different operating conditions. To address this, TCRC...

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Main Authors: Baheta Aklilu T., Hailegiorgis Sintayehu M., Oumer Ahmed N., Sulaiman Shaharin Anwar B
Format: Article
Language:English
Published: EDP Sciences 2018-01-01
Series:MATEC Web of Conferences
Online Access:https://doi.org/10.1051/matecconf/201822505020
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spelling doaj-ff0e528a5ade40779699f75700e640802021-02-02T06:27:34ZengEDP SciencesMATEC Web of Conferences2261-236X2018-01-012250502010.1051/matecconf/201822505020matecconf_ses2018_05020Performance Analysis of Transcritical Carbon Dioxide Rankine Cycle with RegeneratorBaheta Aklilu T.Hailegiorgis Sintayehu M.Oumer Ahmed N.Sulaiman Shaharin Anwar BTranscritical carbon dioxide Rankine cycle (TCRC) has a potential to convert low grade heat source into power. Thus, the objective of this paper is to evaluate TCRC performance based on the first and the second law of thermodynamics for wide and different operating conditions. To address this, TCRC thermal efficiency, exergetic efficiency, utilization ratio and the exergy destruction of the components are analyzed parametrically. Engineering Equation Solver (EES) is used to solve the set of equations and to evaluate the working fluid properties at the given conditions. For the analysis compressor efficiency, turbine efficiency and effectiveness of the regenerator are assumed to be 0.9, 0.9 and 0.95, respectively. The pump inlet pressure was assumed to be 6.2 MPa. It is found that at 10 MPa turbine inlet pressure 240°C is the optimal turbine inlet temperature operating condition. The percentage of exergy destructions at 240°C turbine inlet temperature are 0.94, 4.53, 9.55, 41.23, and 43.74 by the pump, turbine, condenser, heater and regenerator, respectively. Hence, the highest and the smallest exergy destructions are in the regenerator and the pump. This study will help to select the potential component for further improvement.https://doi.org/10.1051/matecconf/201822505020
collection DOAJ
language English
format Article
sources DOAJ
author Baheta Aklilu T.
Hailegiorgis Sintayehu M.
Oumer Ahmed N.
Sulaiman Shaharin Anwar B
spellingShingle Baheta Aklilu T.
Hailegiorgis Sintayehu M.
Oumer Ahmed N.
Sulaiman Shaharin Anwar B
Performance Analysis of Transcritical Carbon Dioxide Rankine Cycle with Regenerator
MATEC Web of Conferences
author_facet Baheta Aklilu T.
Hailegiorgis Sintayehu M.
Oumer Ahmed N.
Sulaiman Shaharin Anwar B
author_sort Baheta Aklilu T.
title Performance Analysis of Transcritical Carbon Dioxide Rankine Cycle with Regenerator
title_short Performance Analysis of Transcritical Carbon Dioxide Rankine Cycle with Regenerator
title_full Performance Analysis of Transcritical Carbon Dioxide Rankine Cycle with Regenerator
title_fullStr Performance Analysis of Transcritical Carbon Dioxide Rankine Cycle with Regenerator
title_full_unstemmed Performance Analysis of Transcritical Carbon Dioxide Rankine Cycle with Regenerator
title_sort performance analysis of transcritical carbon dioxide rankine cycle with regenerator
publisher EDP Sciences
series MATEC Web of Conferences
issn 2261-236X
publishDate 2018-01-01
description Transcritical carbon dioxide Rankine cycle (TCRC) has a potential to convert low grade heat source into power. Thus, the objective of this paper is to evaluate TCRC performance based on the first and the second law of thermodynamics for wide and different operating conditions. To address this, TCRC thermal efficiency, exergetic efficiency, utilization ratio and the exergy destruction of the components are analyzed parametrically. Engineering Equation Solver (EES) is used to solve the set of equations and to evaluate the working fluid properties at the given conditions. For the analysis compressor efficiency, turbine efficiency and effectiveness of the regenerator are assumed to be 0.9, 0.9 and 0.95, respectively. The pump inlet pressure was assumed to be 6.2 MPa. It is found that at 10 MPa turbine inlet pressure 240°C is the optimal turbine inlet temperature operating condition. The percentage of exergy destructions at 240°C turbine inlet temperature are 0.94, 4.53, 9.55, 41.23, and 43.74 by the pump, turbine, condenser, heater and regenerator, respectively. Hence, the highest and the smallest exergy destructions are in the regenerator and the pump. This study will help to select the potential component for further improvement.
url https://doi.org/10.1051/matecconf/201822505020
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