The study on the performance of the gas turbine for power generation

Gas turbines are becoming increasingly used as power generators for a wide variety of applications around the world. Originally they were developed solely for aircraft propulsion where their inherent low specific weight (i.e. mass/unit power) made them essential for high speed flight. For this parti...

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Main Author: Mohd Aidil, Zaini
Format: Undergraduates Project Papers
Language:English
Published: 2008
Subjects:
Online Access:http://umpir.ump.edu.my/id/eprint/491/
http://umpir.ump.edu.my/id/eprint/491/
http://umpir.ump.edu.my/id/eprint/491/1/THE_STUDY_ON_THE_PERFORMANCE_OF_THE_GAS_TURBINE_FOR_POWER_GE.pdf
id ump-491
recordtype eprints
spelling ump-4912015-03-03T06:03:45Z http://umpir.ump.edu.my/id/eprint/491/ The study on the performance of the gas turbine for power generation Mohd Aidil, Zaini TJ Mechanical engineering and machinery Gas turbines are becoming increasingly used as power generators for a wide variety of applications around the world. Originally they were developed solely for aircraft propulsion where their inherent low specific weight (i.e. mass/unit power) made them essential for high speed flight. For this particular purpose they have been developed to a high degree of efficiency both thermodynamically and mechanically. The significant of this study is to increase the performance of the gas turbine in term of the efficiency. The lower efficiency of the gas turbine will effect to the performance of the gas turbine itself, the waste of the fuel because of the unburned hydrocarbon and the impact to the environment, while the gas turbine with a incomplete combustion. To increase the performance in term of efficiency, the gas generator speed is controlled from 1500 rotary per second to 1250 rotary per second. In order to increase the efficiency of the gas turbine, the power output must high, because it is proportional to the efficiency. Besides low fuel consumption is also important to evaluate an efficient gas turbine because it is inversely proportional to efficiency of the unit. From the experiment, is at a speed of 1400 rotary per second, it is the optimum speed that make the gas turbine running at the highest efficiency. The fuel rate consumption at this speed is 1.48E-03kg/s and the power produce is 905.04W. In conclusion, the optimum speed to run the unit at a high efficiency is at 1400 rotary per second which has produced high power output and low fuel consumption. As a recommendation, to further improve the overall performance of the gas turbine unit, air to fuel ratio must be analyzed, in order to find an optimum air to fuel ratio in the combustion chamber. 2008-03 Undergraduates Project Papers NonPeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/491/1/THE_STUDY_ON_THE_PERFORMANCE_OF_THE_GAS_TURBINE_FOR_POWER_GE.pdf Mohd Aidil, Zaini (2008) The study on the performance of the gas turbine for power generation. Faculty of Chemical & Natural Resources Engineering, Universiti Malaysia Pahang. http://iportal.ump.edu.my/lib/item?id=chamo:31315&theme=UMP2
repository_type Digital Repository
institution_category Local University
institution Universiti Malaysia Pahang
building UMP Institutional Repository
collection Online Access
language English
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Mohd Aidil, Zaini
The study on the performance of the gas turbine for power generation
description Gas turbines are becoming increasingly used as power generators for a wide variety of applications around the world. Originally they were developed solely for aircraft propulsion where their inherent low specific weight (i.e. mass/unit power) made them essential for high speed flight. For this particular purpose they have been developed to a high degree of efficiency both thermodynamically and mechanically. The significant of this study is to increase the performance of the gas turbine in term of the efficiency. The lower efficiency of the gas turbine will effect to the performance of the gas turbine itself, the waste of the fuel because of the unburned hydrocarbon and the impact to the environment, while the gas turbine with a incomplete combustion. To increase the performance in term of efficiency, the gas generator speed is controlled from 1500 rotary per second to 1250 rotary per second. In order to increase the efficiency of the gas turbine, the power output must high, because it is proportional to the efficiency. Besides low fuel consumption is also important to evaluate an efficient gas turbine because it is inversely proportional to efficiency of the unit. From the experiment, is at a speed of 1400 rotary per second, it is the optimum speed that make the gas turbine running at the highest efficiency. The fuel rate consumption at this speed is 1.48E-03kg/s and the power produce is 905.04W. In conclusion, the optimum speed to run the unit at a high efficiency is at 1400 rotary per second which has produced high power output and low fuel consumption. As a recommendation, to further improve the overall performance of the gas turbine unit, air to fuel ratio must be analyzed, in order to find an optimum air to fuel ratio in the combustion chamber.
format Undergraduates Project Papers
author Mohd Aidil, Zaini
author_facet Mohd Aidil, Zaini
author_sort Mohd Aidil, Zaini
title The study on the performance of the gas turbine for power generation
title_short The study on the performance of the gas turbine for power generation
title_full The study on the performance of the gas turbine for power generation
title_fullStr The study on the performance of the gas turbine for power generation
title_full_unstemmed The study on the performance of the gas turbine for power generation
title_sort study on the performance of the gas turbine for power generation
publishDate 2008
url http://umpir.ump.edu.my/id/eprint/491/
http://umpir.ump.edu.my/id/eprint/491/
http://umpir.ump.edu.my/id/eprint/491/1/THE_STUDY_ON_THE_PERFORMANCE_OF_THE_GAS_TURBINE_FOR_POWER_GE.pdf
first_indexed 2023-09-18T21:52:46Z
last_indexed 2023-09-18T21:52:46Z
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