TY - JOUR
T1 - Enhancing Part-Load performance of the simple recuperated supercritical carbon dioxide cycle through shaft separation
AU - Son, Seongmin
N1 - Publisher Copyright:
© 2024 Elsevier Ltd
PY - 2024/12
Y1 - 2024/12
N2 - In this study, the operability of a simple recuperated supercritical carbon dioxide (S-CO2) cycle under off-design conditions, specifically during part-load operation, was quantitatively analyzed by implementing shaft separation to place a compressor-driving turbine (CDT). For off-design evaluation, both the heat exchanger and turbomachinery were designed in one dimension before being inserted into the off-design platform of the system. To ensure physical consistency, all turbines were designed using the same set of loss models. The analysis results revealed that the efficiency of the single-shaft configuration decreased by about 12 %p at 10 % output, while that of the separated-shaft configuration decreased by < 8 %p under the same conditions. The arrangement of the CDT and power turbine had minimal impacts on off-design performance. The power required to drive the CDT–compressor operating at the optimal Revolution Per Minuate was found to be less than 5 % of the design output. These findings imply that layout modifications can enhance overall off-design efficiency and that the incorporation of a motor that supplies about 5 % of the design output for the CDT–compressor set significantly improves part-load operability. This requirement is practical, as such a motor is typically required for startup procedures. Although these results were obtained from the simplest recuperated S-CO2 cycle, similar approaches could enhance off-design performance in more complex cycles such as waste heat recovery or S-CO2 recompression cycles. The findings of this study demonstrate that altering the shaft arrangement while considering off-design operability can significantly enhance the operability of S-CO2 systems.
AB - In this study, the operability of a simple recuperated supercritical carbon dioxide (S-CO2) cycle under off-design conditions, specifically during part-load operation, was quantitatively analyzed by implementing shaft separation to place a compressor-driving turbine (CDT). For off-design evaluation, both the heat exchanger and turbomachinery were designed in one dimension before being inserted into the off-design platform of the system. To ensure physical consistency, all turbines were designed using the same set of loss models. The analysis results revealed that the efficiency of the single-shaft configuration decreased by about 12 %p at 10 % output, while that of the separated-shaft configuration decreased by < 8 %p under the same conditions. The arrangement of the CDT and power turbine had minimal impacts on off-design performance. The power required to drive the CDT–compressor operating at the optimal Revolution Per Minuate was found to be less than 5 % of the design output. These findings imply that layout modifications can enhance overall off-design efficiency and that the incorporation of a motor that supplies about 5 % of the design output for the CDT–compressor set significantly improves part-load operability. This requirement is practical, as such a motor is typically required for startup procedures. Although these results were obtained from the simplest recuperated S-CO2 cycle, similar approaches could enhance off-design performance in more complex cycles such as waste heat recovery or S-CO2 recompression cycles. The findings of this study demonstrate that altering the shaft arrangement while considering off-design operability can significantly enhance the operability of S-CO2 systems.
KW - Off-design analysis
KW - Part-load operation
KW - Shaft configuration
KW - Simple recuperated cycle
KW - Supercritical CO
KW - Turbomachinery
UR - http://www.scopus.com/inward/record.url?scp=85210304727&partnerID=8YFLogxK
U2 - 10.1016/j.tsep.2024.103074
DO - 10.1016/j.tsep.2024.103074
M3 - Article
AN - SCOPUS:85210304727
SN - 2451-9049
VL - 56
JO - Thermal Science and Engineering Progress
JF - Thermal Science and Engineering Progress
M1 - 103074
ER -