Investigation of leakage flow in compressor clearances

Rising global temperatures and lower-middle class income levels in recent years have fuelled the energy demand for cooling, which is projected to become a necessity as temperatures continue to rise. It is thus more important than ever to develop sustainable and energy efficient cooling systems. To d...

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Main Author: Lim, Li Ying
Other Authors: Chan Weng Kong
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2020
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Online Access:https://hdl.handle.net/10356/141487
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1414872023-03-04T19:45:09Z Investigation of leakage flow in compressor clearances Lim, Li Ying Chan Weng Kong School of Mechanical and Aerospace Engineering MWKCHAN@ntu.edu.sg Engineering::Mechanical engineering::Fluid mechanics Engineering::Aeronautical engineering Rising global temperatures and lower-middle class income levels in recent years have fuelled the energy demand for cooling, which is projected to become a necessity as temperatures continue to rise. It is thus more important than ever to develop sustainable and energy efficient cooling systems. To do so, one of the key areas of improvement is reducing volumetric inefficiencies in the compressor, which arise as a result of leakages within the compressor chambers. Thus, in this project, leakage flow through clearances in a swing compressor was investigated with the use of Computational Fluid Dynamics (CFD) simulations. The two dominant leakage paths were identified as the end face clearance and radial clearance, which were modelled according to the geometry of the swing compressor of interest. Simulations were conducted at different crank angles and the results were compared to those obtained from a mathematical approach. In addition, for the end face clearance leakage, the effect of additional step clearances was investigated, which was found to increase leakage flow rates by approximately 28%. Parametric studies were also conducted to investigate the effect of varying rotor geometry and pressure ratio on end face leakage, as well as the effect of varying radial clearance height and pressure ratio on radial clearance leakage. Empirical equations were derived for both end face and radial clearance leakages which were found to perform well within the valid range of parameter values investigated. The overall leakage flow rates for the swing compressor was also computed and it was found that the radial clearance was the dominant leakage path in the compressor of interest due to the large clearance heights. Hence, special care should be taken to minimise radial clearances as far as possible to improve overall compressor efficiency. Bachelor of Engineering (Aerospace Engineering) 2020-06-09T01:04:52Z 2020-06-09T01:04:52Z 2020 Final Year Project (FYP) https://hdl.handle.net/10356/141487 en B068 application/pdf Nanyang Technological University
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Mechanical engineering::Fluid mechanics
Engineering::Aeronautical engineering
spellingShingle Engineering::Mechanical engineering::Fluid mechanics
Engineering::Aeronautical engineering
Lim, Li Ying
Investigation of leakage flow in compressor clearances
description Rising global temperatures and lower-middle class income levels in recent years have fuelled the energy demand for cooling, which is projected to become a necessity as temperatures continue to rise. It is thus more important than ever to develop sustainable and energy efficient cooling systems. To do so, one of the key areas of improvement is reducing volumetric inefficiencies in the compressor, which arise as a result of leakages within the compressor chambers. Thus, in this project, leakage flow through clearances in a swing compressor was investigated with the use of Computational Fluid Dynamics (CFD) simulations. The two dominant leakage paths were identified as the end face clearance and radial clearance, which were modelled according to the geometry of the swing compressor of interest. Simulations were conducted at different crank angles and the results were compared to those obtained from a mathematical approach. In addition, for the end face clearance leakage, the effect of additional step clearances was investigated, which was found to increase leakage flow rates by approximately 28%. Parametric studies were also conducted to investigate the effect of varying rotor geometry and pressure ratio on end face leakage, as well as the effect of varying radial clearance height and pressure ratio on radial clearance leakage. Empirical equations were derived for both end face and radial clearance leakages which were found to perform well within the valid range of parameter values investigated. The overall leakage flow rates for the swing compressor was also computed and it was found that the radial clearance was the dominant leakage path in the compressor of interest due to the large clearance heights. Hence, special care should be taken to minimise radial clearances as far as possible to improve overall compressor efficiency.
author2 Chan Weng Kong
author_facet Chan Weng Kong
Lim, Li Ying
format Final Year Project
author Lim, Li Ying
author_sort Lim, Li Ying
title Investigation of leakage flow in compressor clearances
title_short Investigation of leakage flow in compressor clearances
title_full Investigation of leakage flow in compressor clearances
title_fullStr Investigation of leakage flow in compressor clearances
title_full_unstemmed Investigation of leakage flow in compressor clearances
title_sort investigation of leakage flow in compressor clearances
publisher Nanyang Technological University
publishDate 2020
url https://hdl.handle.net/10356/141487
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