Analysis of a recompression supercritical carbon dioxide power cycle with an integrated turbine design/optimization algorithm

被引:39
作者
Saeed, Muhammad [1 ]
Kim, Man-Hoe [1 ]
机构
[1] Kyungpook Natl Univ, Sch Mech Engn, Daegu 41566, South Korea
关键词
Supercritical carbon dioxide cycle simulation; Radial turbine design; Optimization; Recompression Brayton cycle; THERMODYNAMIC ANALYSIS; OPTIMIZATION; PERFORMANCE; DESIGN;
D O I
10.1016/j.energy.2018.09.058
中图分类号
O414.1 [热力学];
学科分类号
摘要
A cycle simulation code with integrated turbine design/optimization algorithm has been developed and utilized for the analysis/optimization of approximate to 10MW(e) recompression supercritical carbon dioxide Brayton cycle. Integrated turbine design and optimization code computes the turbine design engaging the meanline design calculations as a function of received inlet conditions from the main cycle simulation code. Moreover embedded turbine code optimizes the turbine geometric by minimized the losses with in the turbine using response surface optimization methodology and returns turbine geometry and performance parameters to main code. In order to capture the swift variation in thermophysical properties of SCO2 in the supercritical region, cycle design point code and embedded turbine codes are linked with NISI REFPROP program. Integrated turbine design/optimization code was validated using 3D Reynolds Averaged-Navier-Stokes calculations. Response surface methodology was tested by comparing the 3D computation results for the turbine baseline and optimized designs. Finally recompression supercritical carbon dioxide Brayton cycle was analyzed under various conditions of cycle's minimum temperature, minimum pressure, and pressure ratio and split mass fraction. On the basis of the results it is recommended to use proposed model for more realistic and accurate modeling cycle design point analysis. (C) 2018 Elsevier Ltd. All rights reserved.
引用
收藏
页码:93 / 111
页数:19
相关论文
共 43 条
[1]   Response surface method for airfoil design in transonic flow [J].
Ahn, J ;
Kim, HJ ;
Lee, DH ;
Rho, OH .
JOURNAL OF AIRCRAFT, 2001, 38 (02) :231-238
[2]   REVIEW OF SUPERCRITICAL CO2 POWER CYCLE TECHNOLOGY AND CURRENT STATUS OF RESEARCH AND DEVELOPMENT [J].
Ahn, Yoonhan ;
Bae, Seong Jun ;
Kim, Minseok ;
Cho, Seong Kuk ;
Baik, Seungjoon ;
Lee, Jeong Ik ;
Cha, Jae Eun .
NUCLEAR ENGINEERING AND TECHNOLOGY, 2015, 47 (06) :647-661
[3]  
AJ G, 1975, TURBINE DESIGN APPL, V290
[4]   Thermoeconomic analysis & optimization of the combined supercritical CO2 (carbon dioxide) recompression Brayton/organic Rankine cycle [J].
Akbari, Ata D. ;
Mahmoudi, Seyed M. S. .
ENERGY, 2014, 78 :501-512
[5]  
[Anonymous], 2016, World Energy Resources |
[6]  
ANSYS CFX, 2015, ANS CFX PREUS GUID R
[7]  
Aungier R. H., 2006, Turbine Aerodynamics: Axial-Flow and Radial-Flow Turbine Design and Analysis
[8]  
Bergman A.S., 2011, Fundamentals of heat and mass transfer
[9]  
Bradley N, 2007, The Response Surface Methodology
[10]  
Brun K., 2017, FUNDAMENTALS APPL SU