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A Novel Combustion Turbine Inlet Air Cooling System

机译:一种新型燃烧涡轮机入口空冷系统

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Combustion turbine performance is known to significantly deteriorate at elevated ambient temperatures in the Gulf Countries.This phenomenon is typically tackled by incorporating turbine inlet air-cooling systems that are generally classified under evaporative and refrigerative types.Evaporative systems have limited improvement on the turbine performance and add risk of water carryover into the compressor.However,they are simple,require minor modifications to the inlet house,and have low capital and operating costs.On the contrary,refrigerative systems are complex and require high capital and operating costs and also consume significant parasitic power for the water chillers.Nevertheless refrigerative systems guarantee the required inlet air temperature irrespective of the ambient conditions thus,achieve higher power augmentation.This paper introduces a novel system that combines the advantages of both the above technologies.The system basically consists of chiller,cooling tower,inlet air coil,interconnecting piping and controls.The tower works as a primary source of cooling to its maximum capability after which the chiller intervenes to supplement it as a secondary source in order to achieve the desired inlet air temperature that tower solely can not achieve it.The system components are arranged in a manner such that the chiller system alternates between two distinct operational configurations to suit the incurring ambient condition;one is similar to a classical chilled water system while the other is a new arrangement in which cooling is attained by the tower solely or assisted by the chiller.The system guarantees significant increase in power output,reduction of heat rate and exhaust temperature of turbine under various ambient conditions.The system requires smaller chiller that operates less hours and consumes much lower energy than the conventional refrigerative systems.The system also reduces the risks associated with evaporating water into the compressor intake.
机译:已知燃烧涡轮机性能在海湾国家的升高的环境温度下显着恶化。这种现象通常通过掺入涡轮机入口空气冷却系统来解决,所述涡轮机入口空气冷却系统通常在蒸发和制冷类型中进行分类。呼气性系统对涡轮机性能有限有限的改善将含水携带进入压缩机的风险。然而,它们很简单,需要对入口房屋进行微小的修改,并且具有低的资金和运营成本。相反,制冷系统是复杂的,并且需要高的资本和运营成本并消耗很大寄生电力的水冷却器。无论如何都是无论环境条件如何保证所需的入口空气温度,因此实现了更高的功率增强。本文介绍了一种新的系统,这些系统结合了上述技术的优势。系统基本上由冷却器组成。系统基本上由冷却器组成,冷却塔,入口a IR线圈,互连管道和控制器。塔作为其最大能力的初级源作为其最大能力之后,冷却器干预其作为二次来源,以便达到塔的所需的入口空气温度,该塔仅达到塔的所需的入口空气温度。系统部件以这样的方式布置,使得冷却器系统在两个不同的操作配置之间交替以适应产生的环境条件;一个类似于经典的冷冻水系统,而另一个是塔架的新布置,其中塔架达到冷却单独或辅助冷却器。系统保证功率输出的显着增加,在各种环境条件下减少涡轮机的排气温度。该系统需要较小的冷却器,该冷却器运行较少的时间,并且比传统的制冷系统消耗更低的能量。该系统还减少了与蒸发水相关的风险进入压缩机Intak e。

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