Özet
The current study aims at optimisation and comparing the recuperative s-CO2 cycle with the re-compression s-CO2 cycle in case of changes in turbine and compressor isentropic efficiency and TITs. Below 317°C the TIT recuperated Brayton cycle (RBC) has a higher cycle efficiency than RCBC for the case where compressor efficiency is 75% and turbine efficiency is 80%. RBCs with having higher turbomachinery efficiencies (ηc = 85%, ηt = 90%) have higher cycle thermal efficiency than RCBCs with lower turbomachinery efficiencies (ηc = 75%, ηt = 80%). These results will remedy the gap in the literature on information for selecting the appropriate cycle for various purposes under certain thermodynamic inlet conditions.
| Orijinal dil | İngilizce |
|---|---|
| Sayfa (başlangıç-bitiş) | 130-149 |
| Sayfa sayısı | 20 |
| Dergi | International Journal of Exergy |
| Hacim | 32 |
| Basın numarası | 2 |
| DOI'lar | |
| Yayın durumu | Yayınlandı - 2020 |
| Harici olarak yayınlandı | Evet |
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Publisher Copyright:Copyright © 2020 Inderscience Enterprises Ltd.
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