Title of article :
Role of expanders in helium liquefaction cycles: Parametric studies using Collins cycle
Author/Authors :
Thomas، نويسنده , , Rijo Jacob and Ghosh، نويسنده , , Parthasarathi and Chowdhury، نويسنده , , Kanchan، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2011
Pages :
7
From page :
318
To page :
324
Abstract :
Large scale helium liquefaction/refrigeration plant is a key subsystem of fusion devices. Performance of these plants is dependent on a number of geometric and operating parameters of its constituting components such as compressors, heat exchangers, expanders, valves, etc. Expander has been chosen as the subject matter of analyses in the present study. As the sensible cold of helium vapor is lost in liquefiers, the expanders in liquefaction cycles have to provide more refrigeration than those in refrigeration cycles. The expander parameters such as rate of mass flow, operating pressure, inlet temperature, etc. are inter-dependent, and hence, it is difficult to predict the system behavior with variation of a particular parameter. This necessitates the use of process simulators. Parametric studies have been performed on Collins helium liquefaction cycle using Aspen HYSYS®. Collins cycle has all the basic characteristics of a large-scale helium liquefier and the results of this study may be extrapolated to understand the behavior of large scale helium liquefiers. The study shows that the maximum liquid production is obtained when 80% of the compressor flow is diverted through the expanders and it is equally distributed between the two expanders. The relationships between the liquid production and the isentropic efficiency of expanders are almost linear and both the higher and lower temperature expanders exhibit similar trends.
Keywords :
Aspen Hysys® , Refrigeration , Collins helium liquefier , Expander , Parametric study , Thermodynamic efficiency
Journal title :
Fusion Engineering and Design
Serial Year :
2011
Journal title :
Fusion Engineering and Design
Record number :
2357403
Link To Document :
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