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Energetic and Exergetic Analysis of a Transcritical N2O Refrigeration Cycle with an Expander

机译:高临界N2O制冷循环与扩展器的促进分析

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摘要

Comparative energy and exergy investigations are reported for a transcritical N2O refrigeration cycle with a throttling valve or with an expander when the gas cooler exit temperature varies from 30 to 55 °C and the evaporating temperature varies from −40 to 10 °C. The system performance is also compared with that of similar cycles using CO2. Results show that the N2O expander cycle exhibits a larger maximum cooling coefficient of performance (COP) and lower optimum discharge pressure than that of the CO2 expander cycle and N2O throttling valve cycle. It is found that in the N2O throttling valve cycle, the irreversibility of the throttling valve is maximum and the exergy losses of the gas cooler and compressor are ordered second and third, respectively. In the N2O expander cycle, the largest exergy loss occurs in the gas cooler, followed by the compressor and the expander. Compared with the CO2 expander cycle and N2O throttling valve cycle, the N2O expander cycle has the smallest component-specific exergy loss and the highest exergy efficiency at the same operating conditions and at the optimum discharge pressure. It is also proven that the maximum COP and the maximum exergy efficiency cannot be obtained at the same time for the investigated cycles.
机译:比较能量和有效能调查报告用于与节流阀跨临界N2O制冷循环或与膨胀时,气体冷却器出口温度变化范围为30至55℃及蒸发温度变化从-40到10℃。系统的性能还与使用CO 2类似的周期进行比较。结果表明,N2O膨胀循环呈现出较大的最大冷却性能(COP)的系数,降低比CO2膨胀循环和N2O节流阀循环的最佳排放压力。据发现,在N2O节流阀周期,节流阀的不可逆性是最大和气体冷却器和压缩机的能量损失分别第二有序和第三,。在N2O膨胀循环,最大的有效能损失发生在气体冷却器,随后由压缩机和膨胀机。与CO 2膨胀循环和N2O节流阀周期相比,N2O膨胀循环具有最小的特定组件的有效能损失并且在相同的操作条件,并在最佳的排出压力的最高有效能效率。它也证明,最大COP和最大火用效率不能同时为所研究的周期来获得。

著录项

  • 期刊名称 Entropy
  • 作者单位
  • 年(卷),期 2018(20),1
  • 年度 2018
  • 页码 31
  • 总页数 13
  • 原文格式 PDF
  • 正文语种
  • 中图分类
  • 关键词

    机译:N.;

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