期刊文献+

蒸汽压缩热泵压缩机倒置性能试验 被引量:2

EXPERIMENTAL PERFORMANCE OF VAPOR COMPRESSION HEAT PUMP WITH INVERTED COMPRESSOR
下载PDF
导出
摘要 为探究压缩机的倒置性能,搭建性能实验台,研究制冷剂充注量对制冷性能的影响。结果表明:当制冷量及其他条件一定时,随着充注量的增加,压缩机排气温度和功率大于正立的值,制冷COP(coefficient of performance)小于正立的值。最佳制冷剂充注量150 g下的最大制冷COP值为3.2。压缩机倒置后系统性能良好,该系统是"重力无关"系统。压缩机倒置性能实验可为热泵空间应用提供实验参考价值。 Compressor is the core component of the vapor compression heat pump. In order to explore the inverted performance of the vapor compression heat pump compressor, compressor is inverted and performance laboratory bench is built to study the influence of refrigerant charge on system performance. Experimental results show that compressor discharge temperature and compressor power increase with the amount of refrigerant charge under conditions of constant cooling capacity and other conditions. The coefficient of performance (COP) is less than the value obtained when compressor is upright. The maximum cooling COP value of 3.2 under 150 g is got. The cooling performance is good that the vapor compression heat pump can be considered as gravity-independent. Experiments of vapor compression heat pump with compressor inverted provide valuable reference value for space application.
出处 《太阳能学报》 EI CAS CSCD 北大核心 2017年第5期1254-1260,共7页 Acta Energiae Solaris Sinica
基金 研究生科技基金(ykj-2015-11650) 北京市教育委员会科技计划一般项目(KM201610005017)
关键词 蒸汽压缩热泵 倒置压缩机 制冷剂充注量 COP vapor compression heat pump inverted compressor refrigerant charge coefficient of performance (COP)
  • 相关文献

参考文献5

二级参考文献32

  • 1王爱华,梁新刚,任建勋,李明海.航天器变速热泵回路的技术优势分析[J].工程热物理学报,2004,25(S1):147-150. 被引量:2
  • 2赵建福,林海,解京昌,胡文瑞,吕从民,张玉涵.微重力条件下气 /液两相流压降实验研究[J].应用基础与工程科学学报,2001,9(4):373-380. 被引量:11
  • 3王晶,袁卫星,袁修干,余后满.航天领域蒸汽压缩热泵技术研究进展[J].航空学报,2005,26(5):529-534. 被引量:11
  • 4[1]Michael K E.Investigation of lunar base thermal control system o ptions.Society of Automotive Engineers,Paper 932112.
  • 5[2]Scaringe R P.Spacecraft heat pump thermal bus development status & technical issues.Presented by 25th Intersociety Energy Conversion Confe rence,1990.
  • 6[3]Sridhar K R,Ashek Nanjundan.Evaluation of a reverse brayton cycl e heat pump for lunar base cooling. Society of Automotive Engineers,Paper 94127 1.
  • 7[4]Jeffrey H G,Thomas Lovell.High temperature lift heat pump refri g erant and thermodynamic cycle selection.Society of Automotive Engineers,Paper 9 41272.
  • 8[5]Scaringe R P,Buckman J A.Heat pump augmented spacecraft heat rej ection system.Journal of Spacecraft and Rockets,1989,27(3):318—323.
  • 9[6]Sridhar R P.Thermal Control system for lunar base cooling.Journa l of Thermophysics and Heat Transfer,1996,10(3):490—496.
  • 10Ernst Messerschmid,Reinhold Bertrand.Space station:systems and utilization[M].Springer-Verlag Berlin Heidelberg,1999.

共引文献20

同被引文献20

引证文献2

二级引证文献9

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部