Design of centrifugal compressors for heat pump systems

被引:80
作者
Meroni, Andrea [1 ]
Zuhlsdorf, Benjamin [1 ]
Elmegaard, Brian [1 ]
Haglind, Fredrik [1 ]
机构
[1] Tech Univ Denmark, Dept Mech Engn, Nils Koppels Alle,Bldg 403, DK-2800 Lyngby, Denmark
关键词
Turbocompressor; Validation; Preliminary design; Refrigerant; High-temperature heat pump; THERMODYNAMIC ANALYSIS; OPTIMIZATION; REFRIGERANTS; EFFICIENCY; FLOW;
D O I
10.1016/j.apenergy.2018.09.210
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
This work presents a mean-line model of a centrifugal compressor and a method for a coupled optimization with a heat pump system. The compressor model was validated with five test cases from the open literature including the working fluids: air, refrigerant R-134a and carbon dioxide. Afterwards, the compressor model was coupled and optimized with that of a heat pump cycle supplying steam at 150 degrees C. Two cycle configurations were considered: an open-loop system using steam, and a closed-loop system with five other working fluid candidates. The compressor was designed using a multi-objective optimization algorithm, which seeks to maximize simultaneously the cycle coefficient of performance and the supplied heat flow rate. The method employed in this work considers the possible trade-offs regarding cycle and compressor design criteria, and can be used to identify cost-effective solutions for the next generation of heat pumps. The obtained results suggest that a two-stage compressor using steam yields the highest values of coefficient of performance and heat supply, and at the same time requires a more challenging compressor design.
引用
收藏
页码:139 / 156
页数:18
相关论文
共 80 条
[1]  
[Anonymous], 22 INT COMPR ENG C P
[2]  
[Anonymous], 12 IIR GUST LOR C NA
[3]  
[Anonymous], CANADIAN AERONAUTICS
[4]  
[Anonymous], 2016, ECEEE IND SUMM STUD
[5]  
[Anonymous], 47 AIAA AER SCI M IN
[6]  
[Anonymous], 2015, 8 EHPA EUROPEAN HEAT
[7]  
[Anonymous], 12 IEA HEAT PUMP C J
[8]  
[Anonymous], R D J
[9]  
[Anonymous], 24 IIR INT C REFR AU
[10]  
[Anonymous], ASME TURB EXP 2012 T