Research and Development of Supercritical Carbon Dioxide Coal-Fired Power Systems

2020 ◽  
Vol 29 (3) ◽  
pp. 546-575 ◽  
Author(s):  
Zhaozhi Li ◽  
Xuejiao Liu ◽  
Yingjuan Shao ◽  
Wenqi Zhong
Author(s):  
Alessandro Romei ◽  
Paolo Gaetani ◽  
Andrea Giostri ◽  
Giacomo Persico

Abstract The successful penetration of supercritical carbon dioxide (sCO2) power systems in the energy market largely depends on the achievable turbomachinery performance. The present study illustrates a systematic framework where both the compressor and the turbine are designed via validated (within ±2% pts against experiments) mean-line tools and the related impact on cycle performance estimates is quantitatively and qualitatively assessed. A significant effort is devoted to the analysis of centrifugal compressor performance operating close to the critical point, where sharp thermodynamic property variations may make critical the compression process. The analysis is performed for different compressor sizes and pressure ratios, showing a comparatively small contribution of compressor-intake fluid conditions to the machine efficiency, which may achieve technological competitive values (82 ÷ 85%) for representative full-scale sizes. Two polynomial correlations for both turbomachinery efficiencies are devised as a function of proper similarity parameters accounting for machine sizes and loadings. Such correlations can be easily embedded in power cycle optimizations, which are usually carried out assuming constant-turbomachinery efficiency, thus ignoring the effects of plant size and cycle operating parameters. Efficiency correlations are finally exploited to perform several optimizations of a recompressed sCO2 cycle, by varying multiple cycle parameters (i.e. maximum and minimum temperature, pressure ratio and net power output). The results highlight that the replacement of constant-efficiency assumption with the proposed correlations leads to more accurate performance predictions (i.e. cycle efficiency can differ by more than 4% pts), showing in particular that an optimal pressure ratio exists in the range 2 ÷ 5 for all the investigated configurations.


Author(s):  
Robert J. Bruckner

Advanced closed loop power generation cycles are under consideration for a variety of terrestrial and aerospace power systems [1]. High pressure closed brayton cycles (CBC) and supercritical cycles (SCS) offer an advantage where the cycle working fluid can also be used as the lubricant for the fluid film bearings that support the high speed turbomachinery. Unfortunately the use of supercritical carbon dioxide as a lubricant is not well understood. In the supercritical condition fluids that are typically thought of as ideal gases take on a significantly different characteristic. While these fluids typically maintain gas-like absolute viscosities, their densities are liquid like. The combination of these effects leads to the emergence of inertial effects in fluid film bearings. In addition to the inertial effects that are brought on by the high fluid density, the temperature of the lubricant cannot be controlled independently of the thermodynamic process. This situation leads to technical challenges in maintaining dimensional stability and clearance control between the rotating and stationary surfaces of the bearings.


2020 ◽  
Vol 142 (7) ◽  
Author(s):  
Alessandro Romei ◽  
Paolo Gaetani ◽  
Andrea Giostri ◽  
Giacomo Persico

Abstract The successful penetration of supercritical carbon dioxide (sCO2) power systems in the energy market largely depends on the achievable turbomachinery efficiencies. The present study illustrates a systematic framework where both the compressor and the turbine are designed via validated (within ±2% pts against experiments) mean-line tools, and the subsequent impact on cycle performance estimates is quantitatively and qualitatively assessed. A significant effort is devoted to the analysis of centrifugal compressors that operate close to the thermodynamic critical point, where sharp variations in the thermodynamic properties may make the compression process critical. The analysis is performed for different compressor sizes and pressure ratios, showing a comparatively small contribution of the compressor-intake fluid conditions to the machine efficiency, which may achieve competitive values (82–85%) for representative full-scale sizes. Two polynomial correlations for both the turbomachinery efficiencies are devised as a function of proper similarity parameters accounting for machine sizes and loading. Such correlations can be easily embedded in power cycle optimizations, which are usually carried out assuming constant turbomachinery efficiencies, thus ignoring the effects of plant size and cycle operating parameters. Efficiency correlations are finally exploited to perform several optimizations of a representative recompression sCO2 cycle, by varying multiple cycle parameters, namely maximum and minimum temperature, pressure ratio, and net power output. The results highlight that the replacement of the constant-efficiency assumption with the proposed correlations leads to more accurate performance predictions (e.g., cycle efficiency can differ by more than 4% pts), besides demonstrating that an optimal pressure ratio exists in the range 2–5 for all the investigated configurations.


2021 ◽  
Vol 11 (5) ◽  
pp. 2389
Author(s):  
Khaled Alawadhi ◽  
Abdullah Alfalah ◽  
Bashar Bader ◽  
Yousef Alhouli ◽  
Ahmed Murad

The rising environmental problems due to fossil fuels’ consumption have pushed researchers and technologists to develop sustainable power systems. Due to properties such as abundance and nontoxicity of the working fluid, the supercritical carbon (sCO2) dioxide Brayton cycle is considered one of the most promising technologies among the various sustainable power systems. In the current study, a mathematical model has been developed and coded in Matlab for the recompression of the supercritical carbon dioxide Brayton cycle sCO2-BC. The real gas properties of supercritical carbon dioxide (sCO2) were incorporated into the program by pairing the NIST’s Refporp with Matlab© through a subroutine. The impacts of the various designs of the cycle’s individual components have been investigated on the performance of sCO2−BC. The impact of various sedative cycle parameters, i.e., compressor’s inlet temperature (T1), and pressure (P1), cycle pressure ratio (Pr), and split mass fraction (x), on the cycle’s performance (ηcyc) were studied and highlighted. Moreover, an optimization study using the genetic algorithm was carried out to find the abovementioned cycle’s optimized values that maximize the cycle’s per-formance under provided design constraints and boundaries.


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