02676nam a2200229 a 4500 vtls000031315 KUKTEM 20251114204517.0 080829t2008 my a f m 000 0 eng|d THE0003567(Local) 201905152117 zulaiha 201204091018 Fida 201107132241 VLOAD 200908141515 VLOAD 200808291028 ida84 UMP TJ778 .A33 2008 rs Thesis Mohd Aidil Zaini The study on the performance of the gas turbine for power generation / Mohd Aidil Zaini Kuantan, Pahang : UMP, 2008 31 p. : ill. ; 30 cm. + 1 CD-ROM Project paper (Bachelor of Chemical Engineering) --- Universiti Malaysia Pahang - 2008 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.-Author Gas-turbines Performance 0 0 0 1 10000 10000 2019-09-04 0 TJ778 .A33 2008 rs Thesis 0000031377 2019-09-04 00:00:00 1 2019-09-04 PSM 0 0 0 1 10000 10000 2019-09-04 0 CD 2752 | TJ778 .A33 2008 rs Thesis 0000031378 2019-09-04 00:00:00 1 2019-09-04 PSM VIRTUA40 3295 3301 VTLSSORT0080*0200*0400*0900*1000*2450*2600*3000*5020*5200*6500*9992