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Author:

Wang, Xijun (Wang, Xijun.) | Wang, Shunsen (Wang, Shunsen.) | Wu, Chuang (Wu, Chuang.) | Liu, Yuting (Liu, Yuting.) | Sun, Xingye (Sun, Xingye.) | Chen, Da (Chen, Da.)

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Abstract:

To improve the efficiency of the shipborne gas turbine and reduce the temperature of exhaust gas, a novel waste heat recovery cycle composed of supercritical carbon dioxide regenerator Brayton cycle and organic flash cycle is proposed, in which the supercritical carbon dioxide recycles the high temperature exhaust gas, and the organic flash cycle recovers the low temperature exhaust gas. Then, thermodynamic analysis of the cycle and optimization of the target function with cyclic net power are conducted. The results show that under the basic conditions, the thermal efficiency and enthalpy efficiency of the gas turbine after the waste heat recovery cycle are up to 50.4% and 68.93%, which is 44% and 43.6% higher than that of the stand-alone gas turbine cycle, respectively. In addition, the largest value of exergy loss is 842.04 kW in the condenser, accounting for 6% of the system total exergy value. When the carbon dioxide compression pressure ratio is larger and the terminal temperature difference between the heater 1 and heater 2 is smaller, the organic flash cycle evaporation temperature is at the optimum value, and the net power of the cycle is the largest. The largest value of net power is 9 759.64 kW and the final temperature of exhaust gas can be reduced to 177.6 when using p-xylene. © 2019, Editorial Office of Journal of Xi'an Jiaotong University. All right reserved.

Keyword:

Brayton cycle Carbon dioxide Efficiency Exergy Gases Gas turbines Optimization Ships Supercritical fluid extraction Temperature Thermoanalysis Waste heat Waste heat utilization

Author Community:

  • [ 1 ] [Wang, Xijun]Institute of Turbomachinery, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 2 ] [Wang, Shunsen]Institute of Turbomachinery, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 3 ] [Wu, Chuang]Institute of Turbomachinery, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 4 ] [Liu, Yuting]Institute of Turbomachinery, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 5 ] [Sun, Xingye]Institute of Turbomachinery, Xi'an Jiaotong University, Xi'an; 710049, China
  • [ 6 ] [Chen, Da]Institute of Turbomachinery, Xi'an Jiaotong University, Xi'an; 710049, China

Reprint Author's Address:

  • [Wang, Shunsen]Institute of Turbomachinery, Xi'an Jiaotong University, Xi'an; 710049, China;;

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Source :

Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University

ISSN: 0253-987X

Year: 2019

Issue: 11

Volume: 53

Page: 71-78

Cited Count:

WoS CC Cited Count: 0

SCOPUS Cited Count: 6

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 43

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