2020
DOI: 10.1016/j.enconman.2020.113136
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Performance analysis and multi-objective optimization of an integrated gas turbine/supercritical CO2 recompression/transcritial CO2 cogeneration system using liquefied natural gas cold energy

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Cited by 62 publications
(6 citation statements)
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“…Air compressor (AC) [26,33] Z AC = 7900 (P AC ) 0.62 Air turbine (AT) [26,33] Z AT = 1100 (P AT ) 0.81 Cryo-turbine (CT) [26,33] Z CT = 1100(P CT ) 0.81 Inter-cooler (IC) [6] Z IC = 12, 000(A IC /100) 0.6 Condenser (CON) [6] Z CON = 32, 800(A CON /80) 0.68 Evaporator (EVA) [6] Z EVA = 32, 800(A EVA /80) 0.68 Re-heater (RH) [6] Z RH = 12, 000(A RH /100) 0.6 Superheater (SH) [6] Z SH = 12, 000(A SH /100) 0.6 Liquid air tank (LAT) [6] Z LAT = 320 × V LAT Liquid methanol tank (LMT) [33] Z LMT = 572 × V LMT Liquid propane tank (LPT) [33] Z LPT = 1326 × V LPT Liquid thermal oil tank (LOT) [33] Z LOT = 423 × V LOT Liquid air pump (LAP) [33] Z LAP = 483P LAP LNG pump (LNGP) [28] Z LNGP = 1120 (P LNGP ) 0.8 Combustion chamber (CRV) [34] Z CRV = 25.65•m CRV 0.995−p CRV,out /p CRV,in 1 + e (0.018•T CRV,out −26.4) Flue gas turbine (GT) [34] Z GT = 1100 (P GT ) 0.81 Air throttle valve (ATV) [6] Z ATV = 114.5 (m ATV ) 0.67 Separator (SEP) [6] Z SEP = 114.5 (m SEP ) 0.67 Table 3. Investment cost models for the materials.…”
Section: Equipment Model (Usd)mentioning
confidence: 99%
“…Air compressor (AC) [26,33] Z AC = 7900 (P AC ) 0.62 Air turbine (AT) [26,33] Z AT = 1100 (P AT ) 0.81 Cryo-turbine (CT) [26,33] Z CT = 1100(P CT ) 0.81 Inter-cooler (IC) [6] Z IC = 12, 000(A IC /100) 0.6 Condenser (CON) [6] Z CON = 32, 800(A CON /80) 0.68 Evaporator (EVA) [6] Z EVA = 32, 800(A EVA /80) 0.68 Re-heater (RH) [6] Z RH = 12, 000(A RH /100) 0.6 Superheater (SH) [6] Z SH = 12, 000(A SH /100) 0.6 Liquid air tank (LAT) [6] Z LAT = 320 × V LAT Liquid methanol tank (LMT) [33] Z LMT = 572 × V LMT Liquid propane tank (LPT) [33] Z LPT = 1326 × V LPT Liquid thermal oil tank (LOT) [33] Z LOT = 423 × V LOT Liquid air pump (LAP) [33] Z LAP = 483P LAP LNG pump (LNGP) [28] Z LNGP = 1120 (P LNGP ) 0.8 Combustion chamber (CRV) [34] Z CRV = 25.65•m CRV 0.995−p CRV,out /p CRV,in 1 + e (0.018•T CRV,out −26.4) Flue gas turbine (GT) [34] Z GT = 1100 (P GT ) 0.81 Air throttle valve (ATV) [6] Z ATV = 114.5 (m ATV ) 0.67 Separator (SEP) [6] Z SEP = 114.5 (m SEP ) 0.67 Table 3. Investment cost models for the materials.…”
Section: Equipment Model (Usd)mentioning
confidence: 99%
“…For high-temperature heat sources, a sCO 2 cycle can be integrated with a tCO 2 cycle. Su et al (Su et al, 2020) designed such a sCO 2 -tCO 2 combined system for the waste heat recovery of a gas turbine. The heat sink was an LNG.…”
Section: Combined Power Cyclementioning
confidence: 99%
“…[ 1 ] The cryogenic power generation cycle has been considered one of the most preferred methods and has received extensive attention. Su et al [ 16 ] proposed a novel power/cooling cogeneration system driven by LNG cold energy, which consists of a transcritical CO 2 power system, a supercritical CO 2 recompression power system, and a gas turbine. The thermodynamic analysis showed that the combined exergy efficiency and the combined thermal efficiency can reach 30.27% and 52.94%, respectively.…”
Section: Introductionmentioning
confidence: 99%