节点文献

CO2跨临界两级压缩及膨胀机循环的性能分析

Performance Analysis of Transcritical CO2 Two-Stage Compression and Expander Cycle

  • 推荐 CAJ下载
  • PDF下载
  • 不支持迅雷等下载工具,请取消加速工具后下载。

【作者】 杨俊兰; 马一太; 李敏霞; 管海清; 李丽新;

【Author】 YANG Jun-lan, MA Yi-tai, LI Min-xia, GUAN Hai-qing, LI Li-xin (School of Mechanical Engineering, Tianjin University, Tianjin 300072 , China)

【机构】 天津大学机械工程学院; 天津大学机械工程学院 天津 300072; 天津 300072;

【摘要】 为了提高CO2跨临界制冷系统的性能,建立了单级膨胀机循环与4种不带膨胀机的两级压缩循环的数学 模型,并进行了性能计算.结果显示,当膨胀机的效率达到60%时,在给定的气体冷却器出口温度以及蒸发温度范 围内(低于-10 ℃时除外),单级膨胀机循环的性能系数高于两级压缩循环的性能系数.当蒸发温度低于-10℃ 时,带中冷器的两级循环的性能占优势.另外,4种两级压缩循环的排气温度都低于单级膨胀机循环的排气温度.

【Abstract】 In order to improve the performance of the transcritical CO2-refrigeration system, the mathematical models for the single-stage expander cycle and for four types of two-stage compression cycles without expanders were developed and their performance was analyzed. The results showed that the coefficient of the performance of the single-stage expander cycle, when its expander efficiency achieving 60% , was higher than the coefficients of the four two-stage compression cycles within certain ranges of the gas cooler outlet temperatures and the evaporation temperatures (except those less than - 10 ℃). When the evaporation temperature was less than - 10℃, the two-stage cycle with inter-cooler(IC) outperformed the other options. In addition, the discharge temperatures of the four two-stage compression cycles were lower than the temperature of the single-stage expander cycle.

【基金】 国家自然科学基金资助项目(50476060).
  • 【文献出处】 天津大学学报 ,Journal of Tianjin University , 编辑部邮箱 ,2005年11期
  • 【分类号】TB652
  • 【被引频次】9
  • 【下载频次】231
节点文献中: