EFFECT OF INLET AIR COOLING ON THE GAS TURBINE PERFORMANCE USING EVAPORATOR AND VAPOUR ABSORPTION COOLERS AT THE HQ-2 DAUR SSGCL GAS COMPRESSION STATION

Qurban Ali
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Abstract

A gas turbine is a device that converts the energy of fuel into mechanical energy and is used to derive several types of rotating equipment. One of the major drawbacks of a gas turbine is that the performance (power output and thermal efficiency) of a gas turbine decreases instantly with the rise of ambient temperature. At Daur SSGCL Gas Compression Station, gas turbines are used to derive centrifugal type gas compressors to raise the pressure of natural gas where ambient temperature varies between 70 to 500C which decreases the performance of gas turbines. Inlet air cooling is a method through which the effect of ambient temperature on the performance of gas turbines can be decreased. This technique of cooling intake air increases the performance of gas turbines by increasing air density. There are various types of inlet air cooling but, in this study, two types of inlet air cooling techniques are discussed, one of which is wetted media evaporative type and the other one is vapour absorption type. The Evaporative type inlet air cooling technique is suitable for sites with high ambient temperature and low relative humidity and vapour absorption type is used for a wide range of ambient air temperature. In this study, thermodynamic models of the gas turbine have been developed without inlet air cooling (base case/cycle) with inlet air cooling for analyzing the effects of ambient conditions (temperature and relative humidity) on the performance of the gas turbine. The simulated results obtained from Engineering Equation Solver with inlet air cooling systems (vapour absorption and wetted media evaporator cooler) are compared without inlet air cooling (base cycle) gas turbine. On comparison of results of a gas turbine with inlet air cooling systems to without inlet air cooling at ambient conditions, T_0=298.15K (250C) and ∅=60% it is found that gas turbine with evaporator cooler produces 289kW more power than base case/cycle and 390kW more output power with vapour absorption inlet air cooling.
hq-2 daur SSGCL气体压缩站蒸发器和蒸汽吸收冷却器进气冷却对燃气轮机性能的影响
燃气轮机是一种将燃料的能量转化为机械能的装置,用于派生几种类型的旋转设备。燃气轮机的主要缺点之一是燃气轮机的性能(功率输出和热效率)随着环境温度的升高而立即下降。在Daur SSGCL气体压缩站,燃气轮机被用来衍生离心式气体压缩机,以提高天然气的压力,环境温度在70到500摄氏度之间变化,这降低了燃气轮机的性能。进气冷却是一种降低环境温度对燃气轮机性能影响的方法。这种冷却进气的技术通过增加空气密度来提高燃气轮机的性能。进气冷却有多种类型,但本研究主要讨论两种进气冷却技术,一种是湿介质蒸发式,另一种是蒸汽吸收式。蒸发式进风冷却技术适用于环境温度高、相对湿度低的场所,蒸汽吸收式进风冷却技术适用于环境温度范围大的场所。在本研究中,为了分析环境条件(温度和相对湿度)对燃气轮机性能的影响,建立了没有进气冷却的燃气轮机热力学模型(基本工况/循环)。用工程方程求解器对有进气冷却系统(蒸汽吸收和湿介质蒸发器冷却器)的燃气轮机进行了数值模拟,并对无进气冷却(基循环)燃气轮机进行了比较。在环境条件下T_0=298.15K (250C),∅=60%,将有进气冷却系统的燃气轮机与无进气冷却的结果进行比较,发现有蒸发器冷却器的燃气轮机比基准工况/循环多产生289kW的功率,有蒸汽吸收式进气冷却的燃气轮机比基准工况/循环多产生390kW的输出功率。
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