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Preliminary Design of Turbomachinery for the Supercritical Carbon Dioxide Brayton Cycle coupled to the KALIMER-600

机译:结合KALIMER-600的超临界二氧化碳布雷顿循环的涡轮机械的初步设计

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The supercritical CO_2 Brayton cycle has recently been suggested as an alternative power conversion system for a sodium fast reactor in view of its economical efficiency, and a avoidance of the sodium-water reaction. In order to ensure the S-CO_2 energy conversion cycle's efficiency, the efficiency of the turbomachinery is considered first as an important parameter as well as its size. Thus, one-dimensional codes for the turbomachinery have been developed continuously to design and to analyze their performance. For a compressor design, a one-dimensional design and analysis code was developed to determine the compressor configuration parameter near an operation point on the basis of the meanline analysis method and loss models. Using this code, a performance analysis of the S-CO_2 compressor was conducted for the KALIMER-600 S-CO_2 Brayton cycle. In the case of a turbine design, a sensitivity analysis for the performance parameters was conducted by using a one-dimensional code. For the complement of the codes, a three-dimensional flow analysis was conducted for the S-CO_2 turbine with the help of the commercial CFD code.
机译:考虑到超经济的CO 2布雷顿循环的经济效率和避免钠水反应,最近已提出将其作为钠快速反应器的替代功率转换系统。为了确保S-CO_2能量转换循环的效率,首先将涡轮机械的效率及其大小视为一个重要的参数。因此,用于涡轮机械的一维代码一直在不断发展,以设计和分析其性能。对于压缩机设计,基于平均线分析方法和损耗模型,开发了一维设计和分析代码来确定操作点附近的压缩机配置参数。使用此代码,对KALIMER-600 S-CO_2布雷顿循环进行了S-CO_2压缩机的性能分析。在涡轮机设计的情况下,通过使用一维代码对性能参数进行敏感性分析。为了补充这些代码,借助商业CFD代码对S-CO_2涡轮机进行了三维流动分析。

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