Gas Turbine Fouling: A Comparison Among One Hundred Heavy-Duty Frames

Nicola Aldi, N. Casari, Mirko Morini, M. Pinelli, P. R. Spina, A. Suman
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Abstract

Over recent decades, the variability and high costs of the traditional gas turbine fuels (e.g. natural gas), have pushed operators to consider low-grade fuels for running heavy-duty frames. Synfuels, obtained from coal, petroleum or biomass gasification, could represent valid alternatives in this sense. Although these alternatives match the reduction of costs and, in the case of biomass sources, would potentially provide a CO2 emission benefit (reduction of the CO2 capture and sequestration costs), these low-grade fuels have a higher content of contaminants. Synfuels are filtered before the combustor stage, but the contaminants are not removed completely. This fact leads to a considerable amount of deposition on the nozzle vanes due to the high temperature value. In addition to this, the continuous demand for increasing gas turbine efficiency, determines a higher combustor outlet temperature. Current advanced gas turbine engines operate at a turbine inlet temperature of (1400–1500) °C which is high enough to melt a high proportion of the contaminants introduced by low-grade fuels. Particle deposition can increase surface roughness, modify the airfoil shape and clog the coolant passages. At the same time, land based power units experience compressor fouling, due to the air contaminants able to pass through the filtration barriers. Hot sections and compressor fouling work together to determine performance degradation. This paper proposes an analysis of the contaminant deposition on hot gas turbine sections based on machine nameplate data. Hot section and compressor fouling are estimated using a fouling susceptibility criterion. The combination of gas turbine net power, efficiency and turbine inlet temperature (TIT) with different types of synfuel contaminants highlights how each gas turbine is subjected to particle deposition. The simulation of particle deposition on one hundred (100) gas turbines ranging from 1.2 MW to 420 MW was conducted following the fouling susceptibility criterion. Using a simplified particle deposition calculation based on TIT and contaminant viscosity estimation, the analysis shows how the correlation between type of contaminant and gas turbine performance plays a key role. The results allow the choice of the best heavy-duty frame as a function of the fuel. Low-efficiency frames (characterized by lower values of TIT) show the best compromise in order to reduce the effects of particle deposition in the presence of high-temperature melting contaminants. A high-efficiency frame is suitable when the contaminants are characterized by a low-melting point thanks to their lower fuel consumption.
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燃气轮机污垢:100台重型车架的比较
近几十年来,传统燃气轮机燃料(如天然气)的可变性和高成本促使运营商考虑使用低等级燃料来运行重型框架。在这个意义上,从煤、石油或生物质气化中获得的合成燃料可能是有效的替代品。虽然这些替代方案与降低成本相匹配,并且在生物质来源的情况下,可能会提供二氧化碳排放的好处(减少二氧化碳捕获和封存成本),但这些低等级燃料的污染物含量较高。合成燃料在进入燃烧室之前经过过滤,但污染物并没有被完全去除。这一事实导致相当数量的沉积在喷嘴叶片由于高温的值。除此之外,不断提高燃气轮机效率的需求,决定了更高的燃烧室出口温度。目前先进的燃气涡轮发动机在涡轮入口温度为(1400-1500)°C的情况下运行,这个温度足以熔化大部分由低等级燃料引入的污染物。颗粒沉积会增加表面粗糙度,改变翼型形状并堵塞冷却剂通道。与此同时,由于空气污染物能够通过过滤屏障,陆地动力装置会出现压缩机结垢。热段和压缩机污垢共同决定性能下降。本文提出了一种基于机器铭牌数据的热燃气轮机截面污染物沉积分析方法。采用污垢敏感性准则对热段和压缩机污垢进行了估计。燃气轮机的净功率、效率和涡轮入口温度(TIT)与不同类型的合成燃料污染物的结合突出了每个燃气轮机如何受到颗粒沉积。根据污垢敏感性准则,对100台1.2 MW ~ 420 MW燃气轮机进行了颗粒沉降模拟。采用基于TIT和污染物粘度估计的简化颗粒沉积计算,分析了污染物类型与燃气轮机性能之间的相关性。结果允许选择最好的重型框架作为燃料的功能。低效率框架(以较低的TIT值为特征)显示了在高温熔融污染物存在下减少颗粒沉积影响的最佳妥协。当污染物由于其较低的燃料消耗而具有低熔点的特点时,高效框架是合适的。
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