Theoretical Investigation For The Effect of Fuel Quality on Gas Turbine Power Plants

• Published in: Journal of physics. Conference series 2018-05, Vol.1003 (1), p.12022
• Main Authors: khudair, Omar AbdulRazzak, Abass, Khetam Alwan, Abed, Noor Saadi, Ali, Khalid Hussain, AbdulAziz, Saad, Shaboot, Ali Chlaib
• Format: Article
• Language: English
• Subjects: Air masses; Boundary layers; chemical reaction; Chemical reactions; combustion; Combustion chambers; Combustion products; Comparative studies; Discharge; Dividers; flow divider; Fuel combustion; Fuel consumption; Fuel flow; Gas flow; Gas oil; Gas turbine engines; Gas-fired power plants; Gases; Gear pumps; Gear teeth; Mass flow rate; Parameters; Physics; Power consumption; power plant; Power plants; Software; Suction; Surface roughness; Turbine blades
• ISSN: 1742-6588; 1742-6596
• DOI: 10.1088/1742-6596/1003/1/012022

Gas turbine engine power generation is declined dramatically because of the reduction in thermodynamic parameters as a work of turbine, compressor ratio, compressor work, and air mass flow rate and fuel consumption. There are two main objectives of this work, the first is related with the effect of fuel kinds and their quality on the operation of fuel flow divider and its performance specifically gear pump displacement and fuel flow rate to the combustion chambers of gas power plant. AL-DORA gas turbine power plant 35MW was chosen to predict these effects on its performance MATLAB Software program is used to perform thermodynamic calculations. Fuel distribution stage before the process of combustion and as a result of the kind and its quality, chemical reaction will occur between the fuel and the parts of the gear system of each pump of the flow divider, which causes the erosion of the internal pump wall and the teeth of the gear system, thus hampering the pump operation in terms of fuel discharge. The discharge of fuel form the eight external gates of flow divider is decreased and varied when going to the combustion chambers, so that, flow divider does not give reliable mass flow rate due to absence of accurate pressure in each of eight exit pipes. The second objective deals with the stage of fuel combustion process inside the combustion chamber. A comparative study based upon performance parameters, such as specific fuel consumption for gas and gasoil and power generation. Fuel poor quality causes incomplete combustion and increased its consumption, so that combustion products are interacted with the surface of the turbine blades, causing the erosion and create surface roughness of the blade and disruption of gas flow. As a result of this situation, turbulence flow of these gases will increase causing the separation of gas boundary layers over the suction surface of the blade. Therefore the amount of extracted gas will decrease causing retreat work done by turbine, as a result decline of power and gas turbine power plant efficiency causing the drop in the level of electric generation. The fuel quality is found to be a strong function of specific fuel consumption and its effects on the power generation and the efficiency of the gas turbine power plants and hence, the cycle performance shifts towards favorable conditions.