Analysis of an Air Powered Engine System Using a Multi-Stage Radial Turbine

The performance and design criteria of air powered multistage turbines are studied thermodynamically in this paper. In-house code is developed in the C++ environment and the characteristics of four-stage turbines with inter-heating are analyzed in terms of maximum thermal efficiency, maximum exergy...

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Main Authors: Xinjing Zhang, Chunqing Tan, Xiaohui Yan, Haisheng Chen, Xuehui Zhang
Format: Article
Language:English
Published: MDPI AG 2013-03-01
Series:Entropy
Subjects:
Online Access:http://www.mdpi.com/1099-4300/15/4/1186
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author Xinjing Zhang
Chunqing Tan
Xiaohui Yan
Haisheng Chen
Xuehui Zhang
author_facet Xinjing Zhang
Chunqing Tan
Xiaohui Yan
Haisheng Chen
Xuehui Zhang
author_sort Xinjing Zhang
collection DOAJ
description The performance and design criteria of air powered multistage turbines are studied thermodynamically in this paper. In-house code is developed in the C++ environment and the characteristics of four-stage turbines with inter-heating are analyzed in terms of maximum thermal efficiency, maximum exergy efficiency and maximum work output over the inlet temperature range of 293 K–793 K with inlet pressure of 70 bar. It is found that the maximum thermal efficiency, maximum exergy efficiency and maximum work output are 62.6%, 91.9%, 763.2 kJ/s, respectively. However, the thermal efficiency, exergy efficiency and work output are not equivalent for the four-stage radial turbine. It is suggested that at low working temperatures both maximum exergy efficiency and maximum work output can be used as the design objective, however, only maximum work output can be used as the design objective for the four-stage radial turbine over the working temperature range in this work.
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spelling doaj.art-e9f4ea99fbac4128ae7f0da177c110a32022-12-22T04:01:33ZengMDPI AGEntropy1099-43002013-03-011541186120110.3390/e15041186Analysis of an Air Powered Engine System Using a Multi-Stage Radial TurbineXinjing ZhangChunqing TanXiaohui YanHaisheng ChenXuehui ZhangThe performance and design criteria of air powered multistage turbines are studied thermodynamically in this paper. In-house code is developed in the C++ environment and the characteristics of four-stage turbines with inter-heating are analyzed in terms of maximum thermal efficiency, maximum exergy efficiency and maximum work output over the inlet temperature range of 293 K–793 K with inlet pressure of 70 bar. It is found that the maximum thermal efficiency, maximum exergy efficiency and maximum work output are 62.6%, 91.9%, 763.2 kJ/s, respectively. However, the thermal efficiency, exergy efficiency and work output are not equivalent for the four-stage radial turbine. It is suggested that at low working temperatures both maximum exergy efficiency and maximum work output can be used as the design objective, however, only maximum work output can be used as the design objective for the four-stage radial turbine over the working temperature range in this work.http://www.mdpi.com/1099-4300/15/4/1186thermodynamic analysisradial turbinethermal efficiencyexergy efficiencywork output
spellingShingle Xinjing Zhang
Chunqing Tan
Xiaohui Yan
Haisheng Chen
Xuehui Zhang
Analysis of an Air Powered Engine System Using a Multi-Stage Radial Turbine
Entropy
thermodynamic analysis
radial turbine
thermal efficiency
exergy efficiency
work output
title Analysis of an Air Powered Engine System Using a Multi-Stage Radial Turbine
title_full Analysis of an Air Powered Engine System Using a Multi-Stage Radial Turbine
title_fullStr Analysis of an Air Powered Engine System Using a Multi-Stage Radial Turbine
title_full_unstemmed Analysis of an Air Powered Engine System Using a Multi-Stage Radial Turbine
title_short Analysis of an Air Powered Engine System Using a Multi-Stage Radial Turbine
title_sort analysis of an air powered engine system using a multi stage radial turbine
topic thermodynamic analysis
radial turbine
thermal efficiency
exergy efficiency
work output
url http://www.mdpi.com/1099-4300/15/4/1186
work_keys_str_mv AT xinjingzhang analysisofanairpoweredenginesystemusingamultistageradialturbine
AT chunqingtan analysisofanairpoweredenginesystemusingamultistageradialturbine
AT xiaohuiyan analysisofanairpoweredenginesystemusingamultistageradialturbine
AT haishengchen analysisofanairpoweredenginesystemusingamultistageradialturbine
AT xuehuizhang analysisofanairpoweredenginesystemusingamultistageradialturbine