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The energy analysis of GE-F5 gas turbines inlet air-cooling systems by the off-design method

机译:电气F5燃气涡轮机入口空气冷却系统的能量分析通过非设计方法

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Increasing the inlet air temperature causes a reduction in the air mass flow rate, and the efficiency and output power of a gas power plant will reduced. To compensate this power and efficiency decrease, different cooling systems can be applied to the inlet air flow. This paper introduces and analyzes different gas turbine cooling systems and studies their effect on the efficiency of Zanbagh power plant's G11 gas unit by extracting the governing equations regarding the characteristic curve and coding in the MATLAB software. In average, the simulation results show that reduction of 1 degrees C of inlet air temperature between 14 degrees C and 50 degrees C causes an efficiency and power output increase by 0.085% and 0.16 MW, respectively. The maximum cycle efficiency increase applied to cool the inlet air is around 2.7%, which can be achieved using the wet compression method. In addition, this method can reduce fuel consumption by 5% in comparison to a normal cycle.
机译:增加入口空气温度导致空气质量流量的降低,并且燃气发电厂的效率和输出功率将降低。 为了补偿这种功率和效率降低,可以将不同的冷却系统应用于入口空气流量。 本文介绍和分析了不同的燃气轮机冷却系统,并通过提取关于特征曲线的控制方程和Matlab软件编码的控制方程来研究它们对桑巴克发电厂G11气体单元的效率的影响。 平均而言,仿真结果表明,14摄氏度之间的入口空气温度的减小为14℃和50摄氏度之间的效率和功率输出分别增加0.085%和0.16mW。 用于冷却入口空气的最大循环效率增加约为2.7%,可以使用湿式压缩方法实现。 此外,与正常循环相比,该方法可以将燃料消耗降低5%。

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