GPA-C-16S型燃气轮机压气机排气管道新设计的预设计研究结果

S. Ushakov, Аndrey Yurevich Karutsky, O. Shcherbakov, Sergiy Shukov
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本文综述了减少燃气轮机压缩机组污染物排放的设计前研究成果。介绍了乌克兰天然气输送系统使用的压缩机包以及乌克兰公司制造的燃气轮机的污染物排放量。分析了减少燃气轮机污染物排放的主要方法。结果表明,在排气管道中使用特殊的催化剂体系是一种很有前途的方法。为了选择催化剂的位置,对燃气轮机压缩机组GPA-C-16S型排气系统进行了一系列数值模拟。研究表明,排气系统的流动结构复杂,主要是由排气集热器出口的流动特征决定的。研究还发现,涡轮出口气流的旋流引起排气系统气流的显著变化(18%的废气质量流量沿一侧壁面运动,82%沿另一侧壁面运动)。为了防止涡轮出口处的涡流对气流的影响,在排气集热器处采用了特别设计的舌形结构。为了降低整体流动的不均匀性,提出了带管状矫直器的排气管道设计。为了生产GPA-C-16S型的公用热压缩机包,可以配备3.5至9兆瓦的热回收装置。它们的应用可以实现0.36至0.46的热效率。热回收装置可以包含几个独立的热交换器。热回收装置的热功率控制是通过热交换器的开关和通过热交换器的废气流量控制来实现的。热回收装置的设计允许在不关闭燃气轮机的情况下向热交换器注水。为避免高热应力,换热器采用热回收机组冷却系统风扇提供的常压空气进行冷却。
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Results of Pre-Design Studies on the Development of a New Design of the Exhaust Duct of the Gas Turbine Compressor Package GPA-C-16S Type
This article summarizes the results of pre-design studies to reduce pollutant emissions of gas turbine compressor packages. The amount of pollutant emissions of compressor packages used at the Ukrainian gas transmission system as well as gas turbines manufactured by Ukrainian companies is presented. The main methods for reduction in pollutant emissions of gas turbines were analyzed. It was shown that one of the promising methods is to use special catalyst systems in the exhaust ducts. To select the catalyst location, a series of numerical simulations have been performed in the exhaust system of gas turbine compressor package GPA-C-16S type. It was shown that flow in the exhaust system has a complex structure mostly caused by features of the flow at the exhaust collector outlet. It was also found that swirling of the flow at the turbine outlet causes significant change of the flow at the exhaust system (18 % of the mass flow of exhaust gas moves along one of the wall and 82 % along another one). To prevent the degradation of the flow because of swirling at the turbine outlet the especially designed tongue was used at the exhaust collector. To reduce the overall non-uniformity of the flow the exhaust duct design with tubular straightener has been developed. To produce utility heat compressor packages of GPA-C-16S type can be equipped with heat recovery units, of between 3.5 to 9 MW. Their application allows achievement of thermal efficiencies of 0.36 to 0.46. The heat recovery units can contain several separate heat exchangers. Heat power control of the heat recovery units is carried out by heat exchangers on-off and by controlling the flow rate of exhaust gases through them. The design of the heat recovery units allows filling heat exchangers with water without shut-down of the gas turbine. To avoid high thermal stresses heat exchangers are cooled with atmospheric air supplied by fan of the heat recovery unit cooling system.
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