Abstract
Improving energy efficiency and reducing carbon emissions are crucial for the technological advancement of power systems. Various carbon dioxide (CO2) power cycles have been proposed for various applications. For high-temperature heat sources, the CO2 power system is more efficient than the ultra-supercritical steam Rankine cycle. As a working fluid, CO2 exhibits environmentally friendly properties. CO2 can be used as an alternative to organic working fluids in small- and medium-sized power systems for low-grade heat sources. In this paper, the main configurations and performance characteristics of CO2 power systems are reviewed. Furthermore, recent system improvements of CO2 power cycles, including supercritical Brayton cycles and transcritical Rankine cycles, are presented. Applications of combined systems and their economic performance are discussed. Finally, the challenges and potential future developments of CO2 power cycles are discussed. CO2 power cycles have their advantages in various applications. As working fluids must exhibit environmentally-friendly properties, CO2 power cycles provide an alternative for power generation, especially for low-grade heat sources.
Introduction
Carbon dioxide (CO2) was first patented in 1850 as a refrigerant (). In the 1930s and 1940s, with the advent of chlorofluorocarbons (CFCs), CO2 was gradually replaced. At present, environmental protection is a critical requirement in power system design. Therefore, CO2, as a natural working fluid, attracts attention again (). In 1969, Angelino studied the feasibility of applying a CO2 power cycle for nuclear power generation (). Recently, many studies have focused on the CO2 power cycle for high-temperature coal-fired power plants, solar power systems, and low-grade waste heat recovery (Wang et al., 2018b; ).
The average thermal efficiency of standalone CO2 cycles is approximately 40%. However, if a combined cycle is used, the thermal efficiency may rise to 50–60% (). The supercritical CO2 (sCO2) Brayton cycle has the advantages of high efficiency, compact size, and a moderate operation temperature of 400–750°C. However, the sCO2 Brayton cycle is still at an early stage of deployment. Liu et al. () reviewed various sCO2 cycles in terms of working fluid properties, structural configurations, applications, thermodynamic and thermoeconomic performances, experimental systems, and main component designs, including turbines, compressors, and printed circuit heat exchangers (PCHEs). Stein and Buck () presented several advanced CO2 power cycles for concentrated solar power (CSP) applications. Wang et al. (Wang et al., 2017) compared six different system layouts with reheating coupled with a molten salt energy storage system. Wu et al. (Wu et al., 2020) analyzed various sCO2 Brayton cycles for small modular reactors, generation IV reactors, and fusion reactors. White et al. (White et al., 2021) summarized the technical and operational challenges of sCO2 power cycles, including turbomachinery and heat exchanger design, material selection, and optimal operation and control methods. Kumar and Srinivasan () reported the advancements in several transcritical CO2 (tCO2) cycles for solar power generation.
The aforementioned studies primarily focused on sCO2 power cycles or a specific application area. However, recent advancements in system design, the technical challenges, and tCO2 cycles for various applications require further investigation. CO2 power cycles have many different system configurations for different applications. It is necessary to select the most suitable configuration to maximize the performance of a specific application. This paper summarizes the system configurations and operation characteristics of various CO2 power cycles. State-of-the-art technical progress of sCO2 Brayton cycles and tCO2 Rankine cycles are discussed. Applications in combined power systems and economic performance are also discussed. This study can act as a reference for the system design of novel CO2 power cycles.
Thermophysical Properties of CO2
Compared with conventional refrigerants, CO
2as working fluid has the following advantages:
1) non-toxic, non-corrosive, non-flammable, and will not cause an explosion;
2) rich reserves and cost-effectiveness;
3) moderate critical pressure, and good stability in the application temperature range;
4) good compatibility with other materials and lubricants;
5) high density at the supercritical state, small expander volume, and compact heat exchanger;
6) critical temperature and pressure can adapt to a variety of external heat sources;
7) environmentally friendly properties, zero ozone depletion potential (ODP), global warming potential (GWP) is 1;
8) thermodynamic and transport properties of CO2 are known, which are conducive to power cycle design;
9) high thermal stability, high-temperature heat exchanger (directly exchange heat with a heat source to reduce heat loss), low system complexity.
High precision is crucial for the estimation of thermophysical properties. Generally, the Span and Wagner equation of state (EoS) is used, which has an uncertainty of 0.03–0.05% in density, 0.03–1% in the speed of sound, and 0.15–1.5% in heat capacity (; ). Additionally, the EoSs of Kunz and Wagner (), MBWR, and FEQ (Schmidt-Wagner) () can be used to calculate the properties of mixtures containing CO2. Table 1 lists the important thermophysical properties of CO2 at the critical point. A review of the thermodynamic and transport properties of supercritical CO2 can be found in Nikolai et al. (). Because the thermophysical properties of CO2 in subcritical and supercritical states differ significantly, the thermodynamic state of a CO2 power cycle at the pump inlet should be designed accordingly so that it is not too close to the critical point. Figure 1A shows the curves of density, isobaric specific heat capacity, thermal conductivity, and viscosity of CO2 at a pressure of 9 MPa. These properties fluctuated significantly near the critical point. Figure 1B shows the curves of the isobaric specific heat capacity under different pressures. Near the critical point, the specific heat capacity increased rapidly. In power cycles using pure CO2 as the working fluid, impurities in CO2 may affect the performance of the compressor and cooler (Vesely et al., 2019). Therefore, the impurity concentrations should be less than 1%.
TABLE 1
| Property | Value | Unit |
|---|---|---|
| Temperature | 304.13 | K |
| Pressure | 7.3773 | MPa |
| Density | 427.55 | kg/m3 |
| Isobaric specific heat capacity | 1371.9 | kJ/kgK |
| Sound speed | 138.8 | m/s |
| Viscosity | 30.213 | μPaS |
| Thermal conductivity | 337.93 | mW/mK |
Thermophysical properties of CO2 at the critical point.
FIGURE 1
The variations in the thermophysical properties significantly affect the heat transfer calculation. It is important to select an appropriate heat transfer correlation based on the working conditions of CO2. For shell-and-tube heat exchangers, the Krasnoshchekov-Protopopov correlation () can be used. The heat transfer of single-phase CO2 in the subcritical state can be estimated using the Petukhov correlation (). The convective heat transfer coefficient of the gas-liquid flow can be obtained using the Cavallini-Zecchin correlation (). The pressure drop of CO2 in the condenser can be determined using the Kedzierski-Goncalves correlation (). Reznicek et al. () evaluated the predicted error of heat transfer, which was within 5%, and the error in the pressure drop was less than 10%. Recently, PCHEs have been used to exchange heat between supercritical CO2 and high-temperature heat sources. The convective heat transfer coefficient in a PCHE can be calculated using the Gnielinski correlation (; ).
CO2 is not flammable and can be used as a retardant to suppress the flammability of hydrocarbons. Therefore, CO2 is useful for applications with strict safety requirements. Generally, when the mole fraction of CO2 in a mixture reaches 30%, the mixture is non-combustible (). Therefore, some power cycles use zeotropic mixtures containing CO2 and organic fluids to control the flammability while maintaining high efficiency. Mixtures such as CO2/R161(C2H5F), CO2/R1234ze(CF3CH=CHF), and CO2/R134a(CH2FCF3) are not sensitive to variations in the CO2 fraction, while the net power outputs of some mixtures may gradually decrease with an increase in the CO2 fraction (). The CO2 fraction also affects the heat transfer area. The glide temperature should be constrained within a reasonable range. A high glide temperature may cause separation of the mixture and reduce its thermodynamic performance ().
Configurations of CO2 Power Cycles
CO2 power systems are classified as closed supercritical Brayton cycles and transcritical Rankine cycles. Supercritical CO2 is cooled in the sCO2 Brayton cycle, while it is condensed to a subcritical state in the tCO2 Rankine cycle. The performance of the CO2 power cycle can be improved by pre-cooling, intercooling, reheating, pre-compression, and recompression. Generally, sCO2 Brayton cycles are divided into single-flow and split-flow configurations. Figure 2 shows the fundamental single-flow layouts, where recuperation, intercooling, reheating, inter-recuperation, pre-compression, and split expansion are employed. The recuperation configuration can effectively utilize the waste heat at the turbine outlet to improve thermal efficiency. Intercooling can reduce the input power of the compressor. Reheating can increase the expansion work of turbines.
FIGURE 2
The configurations of split-flow sCO2 cycles are shown in Figure 3. Recompression, modified recompression with pre-compression, pre-heating, and five different turbine split-flow configurations are displayed. The cooling pressure of the sCO2 Brayton cycle is greater than 7.38 MPa, leading to a small expansion ratio. However, the temperature at the turbine outlet is still very high. To further improve the utilization efficiency of this part of waste heat, two-stage recuperation and pre-compression can be adopted based on a single-channel configuration or a split-flow configuration with split expansion. For the recompression configuration, a fluid with a low flow rate and high specific heat at the cold side, after the split flow, can exchange heat fully with the fluid with a high flow rate and low specific heat at the hot side inside the low-temperature regenerator. Thus, the pinch-point problem is alleviated, and the system thermal efficiency is improved. For the modified recompression cycle with pre-compression, the working fluid continues to expand to a subcritical state from the turbine outlet to increase the expansion work and then compresses the working fluid to a supercritical state. The working fluid flow is split between the low-temperature recuperator and high-temperature recuperator for the configurations of turbine split flow. Hence, the energy at the outlet of turbine 1 can be comprehensively utilized. For the pre-heating cycle, turbine split flows IV and V, two heaters are installed, which are suitable for applications with two different heat sources.
FIGURE 3

Configurations of split-flow sCO2 Brayton cycles: (A) Recompression; (B) Modified recompression; (C) Pre-heating; (D) Turbine split flow I; (E) Turbine split flow II; (F) Turbine split flow III; (G) Turbine split flow IV; (H) Turbine split flow V (adapted from (
Typical configurations of single-flow and split-flow sCO2 cycles were analyzed in Ahn et al. (
The boundary conditions reported in existing literature for single-flow layouts, including the maximum temperature and pressure, expansion pressure ratio, thermal efficiency, and net power, are listed in Table 2. Figure 4 provides a more intuitive comparison. The diameter of each circle is proportional to the thermal efficiency or net power. The maximum pressure at the turbine inlet was less than 30 MPa, while a maximum pressure of 53.35 MPa was used for theoretical analysis. The maximum temperature was 828°C. Generally, the thermal efficiency improves as the maximum temperature of sCO2 increases. The simple sCO2 cycle has a relatively lower thermal efficiency than the other layouts and is comparable only when the maximum temperature is small. The boundary conditions for the split-flow layouts are presented in Table 3 and Figure 5. The maximum temperature was primarily in the range of 450–650°C, and the maximum pressure was between 20 and 25 MPa. The architectures of these split-flow cycles are complicated and more suitable for large power devices with MW- or even GW-class power output. The results for the thermal efficiency of the recompression cycle cover the range of the other layouts, indicating that the split-flow layouts are well suited for high-temperature applications with a single heat source.
TABLE 2
| Cycle name | Tmax (°C) | pmax (MPa) | PR | ηth (%) | Pnet (MW) | Ref. |
|---|---|---|---|---|---|---|
| Simple | 249 | 19.98 | 2.70 | 14.37 | 22.87 | |
| 145 | 23.94 | 3.03 | 10.71 | 0.73 | ||
| 820 | 20.00 | 2.70 | 14.93 | 0.12 | ||
| 330 | 53.35 | 5.84 | 17.39 | 8.33 | ||
| Recuperation | 320 | 20.00 | 2.56 | 25.00 | 0.14 | |
| 722 | 19.98 | 2.70 | 48.79 | 75.95 | ||
| 600 | 35.00 | 4.00 | 33.05 | 0.10 | ||
| 145 | 17.92 | 2.24 | 11.10 | 0.75 | ||
| 550 | 20.00 | 2.00 | 38.70 | 3.03 | ||
| 330 | 40.00 | 5.38 | 23.20 | 1.67 | ||
| 820 | 20.00 | 2.70 | 44.37 | 0.12 | ||
| 400 | 14.50 | 1.89 | 20.55 | 1.05 | Wang et al. (2020) | |
| 400 | 19.90 | 2.19 | 25.61 | 1.41 | ||
| 350 | 20.00 | 2.56 | 24.80 | 1.00 | ||
| 379 | 27.32 | 3.10 | 29.93 | 2.18 | ||
| 466 | 28.73 | 3.78 | 37.27 | 60.17 | ||
| 500 | 25.00 | 3.33 | 38.03 | 37.97 | ||
| Intercooling | 650 | 20.00 | 2.56 | 43.35 | 8.50 | |
| 145 | 24.74 | 3.12 | 10.62 | 0.72 | ||
| 330 | 40.00 | 5.38 | 22.30 | 1.76 | ||
| 500 | 25.00 | 3.33 | 36.44 | 36.38 | ||
| Reheating | 500 | 25.00 | 3.33 | 39.41 | 39.34 | |
| Interrecuperation | 500 | 25.00 | 3.33 | 39.70 | 39.63 | |
| Precompression | 500 | 25.00 | 3.33 | 40.51 | 40.44 | |
| 550 | 27.00 | 3.00 | 44.44 | 16.00 | Vesely et al. (2019) | |
| 828 | 19.98 | 2.70 | 38.01 | 60.07 | ||
| 572 | 27.58 | 3.05 | 49.04 | 61.21 | ||
| 385 | 27.18 | 3.40 | 31.42 | 2.23 | ||
| Split expansion | 794 | 19.98 | 2.70 | 47.66 | 77.61 | |
| 500 | 25.00 | 3.33 | 34.91 | 34.85 | ||
| Intercooling+recuperation | 145 | 18.33 | 2.25 | 11.51 | 0.78 |
Boundary conditions of sCO2 cycles with single-flow layouts.
FIGURE 4

Boundary conditions of single-flow sCO2 cycles as a function of the maximum operation temperature and pressure: (A) Thermal efficiency; (B) Net power output (legend:
simple
recuperation
intercooling
reheating
inter-recuperation
pre-compression
split expansion
intercooling+recuperation).
TABLE 3
| Cycle name | Tmax (°C) | pmax (MPa) | PR | ηth (%) | Pnet (MW) | Ref. |
|---|---|---|---|---|---|---|
| Recompression | 500 | 25.00 | 3.33 | 43.83 | 43.76 | |
| 811 | 19.98 | 2.70 | 50.87 | 80.92 | ||
| 700 | 20.00 | 2.60 | 53.14 | 293.00 | ||
| 650 | 20.00 | 2.50 | 51.50 | 25.00 | ||
| 600 | 25.00 | 2.63 | 42.90 | 21.42 | ||
| 515 | 25.00 | 2.86 | 42.20 | 479.00 | ||
| 673 | 20.00 | 2.58 | 42.44 | 2184.00 | ||
| 508 | 19.74 | 2.60 | 42.80 | 627.00 | ||
| 550 | 27.00 | 3.00 | 33.44 | 16.00 | Vesely et al. (2019) | |
| 466 | 19.98 | 2.70 | 39.40 | 10.70 | ||
| 550 | 20.70 | 2.80 | 41.48 | 249.00 | Wang and Dai (2016) | |
| 473 | 20.00 | 2.62 | 42.90 | 105.70 | ||
| 570 | 27.58 | 3.40 | 48.46 | 74.20 | ||
| 601 | 25.46 | 3.44 | 46.09 | 7.54 | ||
| 577 | 20.00 | 2.60 | 40.00 | 2.00 | Zhang et al. (2020a) | |
| 310 | 15.00 | 1.88 | 28.50 | 95.27 | Yoon et al. (2012) | |
| 377 | 27.18 | 3.05 | 30.85 | 2.20 | ||
| 450 | 25.00 | 3.13 | 38.96 | 0.025 | Zhang et al. (2020b) | |
| 466 | 28.73 | 3.78 | 41.51 | 52.61 | ||
| 550 | 21.46 | 2.90 | 39.55 | 237.33 | ||
| Modified recompression | 500 | 25.00 | 3.33 | 42.24 | 42.17 | |
| 650 | 20.00 | 2.50 | 47.60 | 25.00 | ||
| Preheating | 500 | 25.00 | 3.33 | 28.24 | 28.20 | |
| 457 | 19.98 | 2.70 | 23.80 | 11.80 | ||
| 307 | 27.72 | 3.52 | 25.97 | 59.75 | ||
| 333 | 27.72 | 3.52 | 27.21 | 70.48 | ||
| 390 | 20.00 | 2.62 | 25.82 | 1.00 | ||
| 352 | 27.32 | 3.04 | 27.30 | 2.75 | ||
| 466 | 28.73 | 3.78 | 37.10 | 61.96 | ||
| Turbine split flow I | 500 | 25.00 | 3.33 | 34.65 | 34.59 | |
| 520 | 20.00 | 2.62 | 28.40 | 1.00 | ||
| Turbine split flow II | 500 | 25.00 | 3.33 | 36.54 | 36.48 | |
| Turbine split flow III | 500 | 25.00 | 3.33 | 31.17 | 31.12 | |
| 551 | 27.86 | 3.56 | 32.76 | 120.92 | ||
| 550 | 20.00 | 2.62 | 26.62 | 1.00 | ||
| 494 | 27.46 | 3.09 | 27.64 | 2.68 | ||
| Modified Split flow III | 507 | 27.58 | 3.53 | 35.66 | 135.16 | |
| Turbine split flow IV | 498 | 27.32 | 3.12 | 29.65 | 2.69 | |
| Turbine split flow V | 399 | 27.46 | 3.05 | 27.49 | 2.74 | |
| Recompression+split expansion | 550 | 27.00 | 3.00 | 29.83 | 16.00 | Vesely et al. (2019) |
| Double recompression | 467 | 19.81 | 2.56 | 39.00 | 95.70 | |
| Two-stage recompression | 700 | 20.00 | 2.60 | 27.14 | 10.00 | Wang et al. (2018b) |
| 550 | 20.00 | 2.60 | 25.04 | 10.00 | Wang et al. (2018c) | |
| Recompression+intercooling | 480 | 19.92 | 2.59 | 39.00 | 96.10 | |
| Recompression+reheating | 415 | 12.44 | 1.61 | 37.00 | 90.60 | |
| 593 | 28.28 | 3.72 | 50.62 | 545.40 | ||
| 593 | 28.28 | 3.72 | 50.64 | 543.30 | ||
| 593 | 28.28 | 3.72 | 50.63 | 560.00 | ||
| Recompression+intercooling+reheating | 620 | 30.00 | 2.43 | 48.37 | 1000.00 | Xu et al. (2018) |
| Turbine split flow III+intercooling | 550 | 27.86 | 3.61 | 32.51 | 122.66 | |
| 494 | 27.46 | 4.10 | 28.61 | 2.77 | ||
| Modified Split flow III+intercooling | 500 | 27.86 | 3.57 | 35.70 | 138.38 | |
| Turbine split flow III +intercooling+preheating | 557 | 27.86 | 3.57 | 36.53 | 142.52 | |
| Preheating+turbine split flow I | 503 | 27.32 | 3.52 | 31.72 | 3.23 | |
| Preheating+turbine split flow I+intercooling | 467 | 27.46 | 3.25 | 30.59 | 3.11 |
Boundary conditions of sCO2 cycles with split-flow layouts.
FIGURE 5

Boundary conditions of split-flow sCO2 cycles as a function of the maximum operation temperature and pressure: (A) Thermal efficiency; (B) Net power output (legend:
recompression
modified recompression
pre-heating
turbine split flow I
turbine split flow II
turbine split flow III
turbine split flow IV
turbine split flow V
combined cycle).
Typical sCO2 cycles are compared in Tables 4, 5. There are four ways to improve the system performance, as shown in Figure 6. The recuperated cycle is a basic improvement of the simple configuration. The recompression cycle and the turbine split flow II are designed to improve the regeneration effect. If the compression process is considered, the intercooling cycle and the inter-recuperated cycle are optimum improvements. The expansion process can be enhanced via the pre-compression cycle or the recompression cycle with pre-compression. If the heating process is considered, the other five configurations can be employed to improve heat transfer. There is no single configuration that is well suited for all applications. During the system design process, specific operation situations, temperatures of the heat source and sink, system size, and cost should be considered. A comparison of different configurations must be performed, and the most appropriate configuration should be chosen.
TABLE 4
| Cycle | Characteristics | Advantages | Disadvantages |
|---|---|---|---|
| Simple | The simplest closed Brayton cycle | Simple configuration, low cost, easy to construct, easy to control | Low thermal efficiency |
| Recuperation | A recuperator is added based on the simple cycle | Simple configuration, relatively high thermal efficiency, low cost, easy to control | Pinch point exists in the recuperator |
| Intercooling | One intercooler is inserted between two compressors | The pressure at the turbine inlet is increased, and the compressor work is reduced | Cooling consumption work is increased |
| Reheating | Dual expansion with one reheater | Utilization of heat source is improved, high expansion work | Suitable for high-temperature heat source |
| Inter-recuperation | Two recuperators and two-stage compression | Pinch-point problem is alleviated, relatively high thermal efficiency | High compression work |
| Pre-compression | One pre-compressor is added before the cooler | The cooling pressure is increased, the pressure at the turbine outlet is decreased | Compression work is increased, the subcritical working process may occur in the turbine and the pre-compressor |
| Split expansion | One turbine is added before the heater | The working pressure of the heater is relatively low | Expansion work may decline, low thermal efficiency |
Comparison of single-flow sCO2 cycles.
TABLE 5
| Cycle | Characteristics | Advantages | Disadvantages |
|---|---|---|---|
| Recompression | Part of the flow is compressed without cooling | Pinch-point problem is alleviated, recuperation improves the efficiency, smaller cooler | Complex compressor arrangement, control is complicated, limited variation of the heat source temperature |
| Recompression cycle with pre-compression | One pre-compressor is added based on the recompression cycle | Expansion work is increased, and the state at the turbine outlet can be subcritical | Complex compressor arrangement, the transcritical working process may occur in the turbine and pre-compressor |
| Pre-heating | Part of the flow is recuperated, and the other part is pre-heated by the heat source | The outlet temperature of the heat source is decreased, suitable for multi-heat sources | The energy of spent gas may not be utilized comprehensively, low thermal efficiency, complex heater arrangement |
| Turbine split flow I | Part of the flow from the compressor is recuperated by the low-temperature recuperator and then enters the heater | The heat source temperature at the heater outlet is decreased, the energy utilization at the HP turbine outlet is increased | Complex system layout, high cost, the temperature at the HP turbine must be high enough |
| Turbine split flow II | Part of the flow from the compressor is recuperated by the HP recuperator and then enters the heater | The energy of the spent gas at the HP turbine outlet is utilized comprehensively | Complex system layout, high cost, the outlet temperature of heat source is limited |
| Turbine split flow III | Part of the flow from the compressor is delivered to the heater directly | The heat source temperature at the heater outlet is decreased, the energy at the HP turbine outlet is utilized comprehensively | Complex system layout, high cost |
| Turbine split flow IV | Each of the split flows is heated by an individual heater, and two recuperators are used | The heat energy from two different sources with distinct temperatures can be fully utilized | Complex system layout, high cost, a complicated control strategy for dynamic heat sources |
| Turbine split flow V | Each of the split flows is heated by an individual heater, and a common recuperator is used | The heat energy of the two sources with distinct temperatures can be fully utilized, and only one recuperator is used | Complex system layout, high cost, a complicated control strategy for dynamic heat sources |
Comparison of split-flow sCO2 cycles.
FIGURE 6

Improvement paths for sCO2 Brayton cycles.
In the tCO2 Rankine cycle, CO2 is condensed through a heat sink. Generally, the tCO2 Rankine cycle is used when the ambient temperature is lower than the critical temperature of CO2. The thermal efficiency of a tCO2 Rankine cycle can approach or even exceed that of a traditional Rankine cycle as the turbine inlet temperature increases. Furthermore, the structure of the CO2 Rankine cycle is simpler and more compact. For low-temperature heat sources, the system configurations of the tCO2 cycle are relatively simple. The boundary conditions reported in the existing literature for tCO2 cycles are listed in Table 6, and are also plotted in Figure 7. The maximum temperature for the simple tCO2 cycle was less than 130°C. However, the temperature range for the recuperation cycle covered a large interval of up to 820°C. Accordingly, the thermal efficiency of the recuperation layout was much higher in the high operation temperature regions. The efficiency of the other cycles showed no evident advantages over the recuperation cycle. At present, most studies on tCO2 cycles are mainly focused on small power devices with a power output of 200–600 kW. The characteristics of the four configurations (
TABLE 6
| Cycle name | Tmax (°C) | pmax (MPa) | PR | ηth (%) | Pnet (MW) | Ref. |
|---|---|---|---|---|---|---|
| Simple | 112 | 12.80 | 1.99 | 8.14 | 3.740 | |
| 95 | 13.60 | 2.67 | 8.40 | 1.034 | ||
| 120 | 11.00 | 3.67 | 12.75 | 0.273 | ||
| 110 | 12.00 | 1.66 | 6.40 | 13.300 | Wang and Dai (2016) | |
| 115 | 14.55 | 2.36 | 8.20 | 0.272 | ||
| 99 | 14.20 | 2.79 | 8.80 | 0.607 | ||
| 130 | 17.78 | 3.10 | 8.21 | 1.910 | Wu et al. (2018) | |
| 820 | 20.00 | 3.13 | 16.68 | 0.155 | ||
| Recuperation | 112 | 12.80 | 1.99 | 8.33 | 3.740 | |
| 95 | 11.30 | 2.22 | 8.60 | 1.379 | ||
| 280 | 17.00 | 2.36 | 30.29 | 6.200 | ||
| 450 | 20.00 | 3.11 | 30.72 | 0.357 | Wang et al. (2018a) | |
| 130 | 14.00 | 2.44 | 8.95 | 2.080 | Wu et al. (2018) | |
| 335 | 13.30 | 8.36 | 28.12 | 0.716 | ||
| 650 | 17.00 | 3.00 | 32.80 | 0.100 | ||
| 272 | 21.70 | 2.52 | 20.20 | 0.515 | ||
| 112 | 11.28 | 2.22 | 8.51 | 0.278 | ||
| 820 | 20.00 | 3.13 | 43.45 | 0.155 | ||
| Regenerative cycle with open-feed heater | 112 | 12.80 | 1.99 | 8.30 | 3.490 | |
| Reheating | 107 | 12.80 | 1.99 | 8.35 | 3.830 | |
| Turbine split flow I | 450 | 20.00 | 3.11 | 28.38 | 0.484 | Wang et al. (2018b) |
| Recompression | 477 | 20.10 | 2.68 | 31.32 | 0.474 | |
| 233 | 21.60 | 2.45 | 17.65 | 0.613 | ||
| Pre-heating | 248 | 21.70 | 2.49 | 16.73 | 0.607 |
Boundary conditions of tCO2 cycles.
FIGURE 7

Boundary conditions of tCO2 cycles as a function of the maximum operation temperature and pressure: (A) Thermal efficiency; (B) Net power output (legend:
simple,
recuperation,
regenerative cycle with open-feed heater
reheating
turbine split flow I
recompression
pre-heating).
TABLE 7
| Cycle | Characteristics | Advantages | Disadvantages |
|---|---|---|---|
| Simple | The simplest closed Rankine cycle | Simple configuration, low cost | Low thermal efficiency, condensation is difficult under high ambient temperature |
| Recuperation | One recuperator is added based on the simple Rankine cycle | Efficiency is improved, smaller condenser | Mass flow rate is increased, leading to a higher pump work |
| Reheating | One reheater and a low-pressure turbine are added | Suitable for relatively high-temperature heat source, expansion work is increased | Complex system configuration, high cost, not suitable for dynamic conditions |
| Regenerative cycle with open-feed heater | An open-feed heater is used | Small condenser and low pump work | Part of the expansion work is lost and relatively low thermal efficiency |
Comparison of tCO2 Rankine cycles for low-temperature sources.
Performance Characteristics of CO2 Power Cycles
The temperature and pressure of supercritical CO2 at the inlet of the high-pressure turbine are the two key parameters affecting the system performance. With an increase in the turbine inlet temperature, the system efficiency gradually increases, especially when the turbine inlet temperature is low (
CO2 turbines have some advantages, such as smaller size, less leakage, and shock loss. The turbine size of a sCO2 cycle is significantly smaller than that of a subcritical organic Rankine cycle (ORC). On the other hand, operating conditions for higher speed and greater pressure require a higher mechanical strength of the turbo-generator, especially for the bearing and seal design. The choice of working fluid also affects the geometric parameters of the turbine (
Air cooling is not suitable for steam Rankine cycles. However, air cooling has some advantages in sCO2 power cycles, such as a smoother temperature match profile, lower exergy loss, smaller corrosion and scale deposition, and sediment accumulation. For CSP systems, the sCO2 cycle using air cooling can save a large amount of water, which is critical in inland regions. When the ambient temperature is high, hybrid cooling combing air and water is another option that can reduce performance degradation (
Applications of sCO2 Cycles
In this section, recent progress in sCO2 cycles in nuclear and coal-fired power plants, waste heat recovery, concentrated solar systems, and geothermal power devices are presented.
Nuclear Reactor
The recuperated sCO2 cycle is often used in high-temperature gas-cooled reactors, which have high thermal efficiency, relatively low turbine inlet temperature, compact size, and simple layout (Yoon et al., 2012;
The recompression sCO2 cycle can be applied to a fourth-generation sodium-cooled fast reactor. Thus, the risk of a chemical reaction between Na and water in the conventional steam Rankine cycle is avoided. KAERI designed a recompression sCO2 cycle based on the KALIMER 600 system. The rated power was 600 MW. Two centrifugal compressors and a four-stage axial turbine were designed. The estimated thermal efficiency was 42.8% (
Supercritical CO2 in a nuclear reactor exhibits very high pressure, which is not conducive to the safety of commercial plants. The working pressure of current nuclear reactors is below 15 MPa although it can be as high as 25 MPa. The maximum working pressure can be decreased by combining the split expansion cycle with the recompression cycle while maintaining a high efficiency level. An investigation showed that the thermal efficiency of the system decreased slightly from 43.88 to 43.11% with a small increase in the heat transfer area, when the inlet temperature of the high-pressure turbine was reduced to 390°C, and the inlet pressure decreased from 20 to 15 MPa (
For the recompression cycle, the temperature at the inlet of the main compressor is higher than that of the recompressor. If the compressors maintain a constant speed, the split ratio declines as the ambient temperature increases, leading to an apparent decrease in performance. Thus, a proper control strategy is required to maintain high performance under off-design conditions (
Coal-fired Power Plant
The steam Rankine cycle is a popular technology used in coal-fired power plants. To improve energy efficiency, an ultra-supercritical steam Rankine cycle with two-stage reheating is under development. However, owing to the limitations of the material and other technical constraints, the efficiency improvement of the ultra-supercritical steam Rankine cycle has stagnated. Investigations suggest that the sCO2 Brayton cycle is a feasible alternative technology. Recently, the application of sCO2 cycles to coal-fired power plants has attracted significant attention. Li et al. reviewed various applications of sCO2 cycles for pulverized coal power plants, circulating fluidized bed devices, and oxy-coal power systems (
The working temperature of the sCO2 cycle for a coal-fired power plant can be as high as 900°C; the recompression cycle is ideal for this. Reheating is also a useful approach in this regard. Zhou et al. (Zhou et al., 2018) analyzed the performance of a recompression cycle with reheating and two-stage intercooling. Compared with the original 1000 MW single-stage reheating ultra-supercritical steam Rankine cycle (605°C/603°C/274 bar), the optimized thermal and exergy efficiencies of the sCO2 cycle reached 47.64 and 81.25%, respectively. However, the flow rate of CO2 increased significantly, resulting in an excessive pressure drop in the heat exchange process in the boiler, which made it difficult to fully utilize the flue gas energy. Xu et al. designed a partial-split strategy to halve the flow rate and length of the heat exchangers in the boiler (Xu et al., 2018). As a result, the overall pressure drop was reduced to 1/8. Furthermore, the exhaust temperature of the flue gas was reduced to below 120°C by diverting part of the working fluid after intercooling to recover the waste heat of the flue gas. Based on this strategy, a 1000 MW sCO2 power generation system was proposed (
Coal-fired power plants are the main source of CO2 emissions. Integration with carbon capture and storage devices is useful for alleviating the greenhouse gas effect. A two-stage cascade sCO2 cycle with a carbon capture unit was evaluated by Olumayegun et al. (
Waste Heat Recovery
A CO2 cycle can be used as the bottom cycle to recover the exhaust heat of a heat engine, such as a gas turbine or internal combustion engine, and the overall energy efficiency can be improved. Hou et al. (
Two typical heat sources exist in an internal combustion engine, that is, exhaust gas and coolant. Novel sCO2 cycles were designed to recover the different types of waste heat. Figure 8 shows the modified recompression sCO2 cycle. Two heat exchangers were installed to recover the waste heat of the exhaust gas in series. The cycle efficiency increased as the inlet temperature of the high-pressure turbine increased, although the net power output decreased. Under the design conditions, the waste heat recovery efficiency was 17.86% greater than that of the recompression cycle, and the optimized heat recovery efficiency reached 74.83% (Zhang et al., 2020b). To recover the exhaust and cooling simultaneously, Song et al. designed a sCO2 cycle with two-stage regeneration, and the maximum output power of the engine was increased by 6.9% (
FIGURE 8

A modified recompression sCO2 cycle for engine waste heat recovery (adapted from (Zhang et al., 2020b)).
Concentrated Solor Power System
The performance of sCO2 cycles has been investigated for high-temperature solar thermal power systems. The thermal efficiency was approximately 32% with a source temperature of 600°C and a compressor inlet pressure of 85 bar (
Solar radiation varies significantly at different times of the day. A heat storage device was installed to alleviate the influence of temperature fluctuations. Wang et al. (Wang et al., 2018c) studied a CSP system with heat storage. The recompression sCO2 cycle was integrated with reheating and intercooling. The solar circuit was coupled with the sCO2 cycle via a heat storage device. A salt mixture (8.1 wt% NaCl + 31.3 wt% KCl + 60.6 wt% ZnCl2) was used in the heat storage device to balance the energy fluctuations of the heat addition process. Based on the radiation data of a typical sunny day in western China, the total photoelectric efficiency could reach 19.17–22.03%, which was higher than that of traditional tower solar systems.
When the power output fluctuates frequently, the performances of the turbine and compressor degrade significantly and may even cause the failure of the control strategy. For every 1% reduction in the turbine efficiency, the system efficiency and relative power output could be decreased by 0.431 and 1.713%, respectively (
A radial turbine can be used in a sCO2 cycle owing to its low expansion ratio. El Samad et al. (
Large-scale high-temperature solar thermal power systems are generally built in desert areas where solar radiation is abundant and air cooling is required (
Geothermal Power Generation
Geothermal sources have a much lower temperature than nuclear reactors and coal-fired power plants. Generally, the tCO2 Rankine cycle is more suitable for low-grade energies. A relatively low condensation temperature is required to ensure the operation of a tCO2 power system. However, it may be difficult to condense CO2 if the ambient temperature is high. Few investigations have evaluated the feasibility of the sCO2 cycle for the utilization of geothermal energy. Ruiz-Casanova et al. (
For high-temperature applications, special attention should be paid to the corrosivity of CO2 and impurities in the system materials. Some materials can form a protective oxide film on the surface, such as chromium oxide and alumina, and have good compatibility with CO2. Haynes 230 (
Several MW-level CO2 experimental systems, which concentrated on simple and recuperated configurations, have been built. More experimental systems need to be developed to validate the theoretical results. Furthermore, during the development of experimental system, technical issues can be discovered, and expertise can be gained aiding future engineering development.
Compared with the conventional steam Rankine cycle, the sCO2 cycle has low critical pressure, high density, high heat transfer rate, high specific power, and small size (
TABLE 8
| Application | Operating conditions | Cycle configuration | Advantages | Challenges | |
|---|---|---|---|---|---|
| Temperature | Pressure | ||||
| Nuclear reactor | 300–600°C | 12–25 MPa | Recompression cycle, double recompression cycle | High thermal efficiency, compact size, simple system layout, intercooling and reheating can improve performance | High operating pressure, system safety, material corrosion |
| Coal-fired power plant | 600–700°C | 20–35 MPa | Recompression cycle with reheating and intercooling, partial-split arrangement of the heater, cascade system consisting of top and bottom cycles | High thermal efficiency, compact size, air cooling is possible, integration with carbon capture system (CCS) | Complicated layout, high operating temperature, turbine manufacturing |
| Waste heat recovery | 320–570°C | 15–25 MPa | Recompression cycle, recompression cycle with split expansion, recuperated cycle, split recuperated cycle | Compact size, environmentally friendly, synergic energy utilization with multi-heat sources | High cost, small-scale turbine design and manufacturing |
| Solar power system | 450–900°C | 25–30 MPa | Recompression cycle, recuperated cycle, recompression with reheating and intercooling | Environmentally friendly, integration with thermal storage, air cooling is possible | Robustness under dynamic working conditions, material corrosion under high-temperature conditions |
| geothermal power system | 60–145°C | 12–16 MPa | Recuperated cycle, recuperated cycle with intercooling | Environmentally friendly, suitable for low-temperature heat source | Sensitive to ambient temperature, state at the turbine inlet close to the critical point |
Characteristics of sCO2 cycles for different applications.
Applications of tCO2 Rankine Cycles
A tCO2 cycle is suitable for low-grade energy utilization if the ambient temperature is lower than 30°C, such as in low-temperature geothermal and solar power generation. Compared with an ORC, a tCO2 cycle takes advantage of its environmentally friendly properties and compact size. The configurations of the tCO2 cycle for low-temperature heat sources are limited, with most focusing on the simple or recuperated cycle. Compared with the working fluids of ethane, toluene, siloxane D4, and water, the exergy efficiency of a simple or regenerative tCO2 cycle is greater, and the system size is smaller; however, the thermal efficiency is lower (
Water cooling is favorable for most applications. The temperature of the geothermal water at the evaporator outlet is generally constrained to over 70°C to prevent the precipitation of silica from geothermal water. Owing to this constraint, the CO2 flow rate decreases gradually with the reduction in cooling water temperature, and the net power output increases at first and then decreases. There is an optimal cooling water temperature that maximizes the net power output. Air cooling is also feasible in cold climate regions. If the cooling water temperature is too high, it is impossible to condense the subcritical CO2. Pan et al. (
At present, Echogen provides commercial products of tCO2 power cycle: EPS100, EPS35, and EPS30 (
There are some disadvantages to tCO2 cycles, including high operating pressure, difficult condensation, and low thermal efficiency. To overcome these disadvantages, a binary mixture consisting of CO2 and an organic working fluid can be used (
Combined Power Cycle
The CO2 power cycle is generally used alone, but it can also be combined with other cycles. Figure 9 shows the possible ways of forming a combined power system based on a sCO2 cycle. According to the principle of synthetically cascaded utilization of energy, a combined power cycle can improve the overall energy efficiency.
FIGURE 9

Possible approaches for the combined system based on sCO2 cycles.
A combined power system can be used for a single heat source. For example, a CO2 power cycle is cascaded with a bottoming ORC. Mondal et al. (
Various types of heat sources may exist in industrial processes. A CO2 power cycle can be cascaded with an ORC or a conventional steam Rankine cycle to fully utilize these different energies. For example, a combined system of the sCO2 cycle and ORC can be designed to reclaim waste heat from engine exhaust and coolant. The topping sCO2 cycle is used to recover the waste heat of the exhaust gas, and the bottoming ORC is used to absorb the heat rejection of the sCO2 cycle, waste heat of the engine coolant, and residual heat of the exhaust gas. The maximum net power output and minimum specific investment cost of the combined system were 58% and 4% higher than those of the single sCO2 power cycle (
A CO2 power cycle can be integrated with other power systems in parallel to form a complex synthetic energy system. For example, a sCO2 cycle was designed for a waste incineration power plant by Hao et al. (
Toshiba proposed a tCO2 cycle combined with an oxy-fuel gas turbine, called the Allam cycle (
Economic Analysis of CO2 Cycle
Economic performance is an important factor affecting decision-making. The conventional model based on chemical engineering plant cost index (CEPCI) is generally employed to estimate the capital cost (
Generally, CO2 power cycles have a higher cost than ORCs, which is the main factor restricting commercial production. Using zeotropic mixtures containing CO2 is a feasible option that can reduce costs while maintaining high efficiency (Xia et al., 2018). At present, few investigations have focused on the economic performance of CO2 power cycles. More efforts are required for various industrial applications to provide a comprehensive comparison among the conventional steam Rankine cycle, ORC, Kalina, and other power systems.
Technical Challenges and Possibilities of Future Development
Although CO2 power cycles have great potential for industrial applications, some technical challenges still need to be overcome. Figure 10 shows the main challenges and possible directions for future development. First, CO2 is a natural working fluid with environmentally friendly characteristics, such as zero ODP and low GWP. However, CO2 is a limiting substance in the occupational exposure limit standard for hazardous factors in the workplace. CO2 with a concentration greater than 2% will cause fatal harm to human beings in a closed space. Generally, the concentration of CO2 prescribed in the hygiene requirements is less than 5000 ppm. Therefore, CO2 gas leakage detection and the formulation of relevant safety specifications are needed to provide safety support for the industrial application of CO2 power cycles.
FIGURE 10

Technical challenges and possible future developments of CO2 power cycles.
The characteristics of fluid flow and heat transfer of supercritical CO2 need to be investigated experimentally such that accurate correlations can be developed for a wide range of CO2 power cycles. PCHEs that can operate under high-pressure and temperature conditions are suitable for applications with a compact size requirement. Flow passage optimization and reduction of pressure drops of PCHEs should be investigated further. Furthermore, CO2 can be used as a flame retardant and blended with an organic working fluid. The thermophysical properties of zeotropic mixtures containing CO2 should be measured to provide accurate data for industrial applications. Thus, a high-fidelity economic model and a comprehensive analysis can be performed.
The energy efficiency of the high-temperature sCO2 power cycle increases with an increase in the maximum working pressure. However, the high operating temperature poses a severe challenge to metal materials. The material strength should be improved, and the wall thickness must be increased. In addition, it is possible to control the maximum working pressure to a reasonable level and improve the system efficiency by reducing the exergy loss of the components. For coal-fired power plants, the design of a high-temperature sCO2 power cycle needs to be considered together with the design of carbon capture and carbon storage devices to meet the carbon neutrality target.
CO2 power cycles take advantages of environmentally friendly properties, low cost, high output power, and are best suited for solar and geothermal sources. For solar power applications, a solar collector with high concentrating performance can enhance the operating temperature and system efficiency. Combining it with a heat storage device can effectively suppress fluctuations in solar energy. Furthermore, it can be integrated with domestic heat supply such that comprehensive energy utilization is realized, and the energy efficiency is improved greatly. This has good prospects in micro-distributed energy supply systems. For low-temperature geothermal power generation, few investigations have focused on the CO2 power system, and more research and engineering developments are needed. A supercritical state is observed for the sCO2 cycle during the cooling process, and air cooling is feasible, especially for areas with water shortages. A tCO2 cycle is more suitable for areas at high latitudes or altitudes with low ambient temperatures or areas with abundant water resources.
The high-pressure and high-temperature operating conditions of CO2 power systems are a severe challenge to the reliability and durability of the system components, which require careful verification in engineering practice. Supercritical CO2 with high density has a significant impact on the high-speed rotating vanes of the turbine and compressor, and the mechanical stress of the blades must be specified in the design. To ensure reliable sealing and improve the compactness of the system, the compressor, alternator, and turbine are designed as an integrated turbine-alternator-compressor (TAC). Generally, high heat loss occurs owing to the heat transfer between the different parts of the TAC. It is necessary to reduce the heat loss of the turbine to a very low level while simultaneously ensuring good cooling of the alternator. The optimal regulation of the compressor and turbine under off-design conditions needs to be further studied.
Conclusion
In this paper, recent advancements in the system design and applications of supercritical/transcritical CO2 power cycles are discussed. Single-flow and split-flow CO2 power cycles have their own advantages. New CO2 power cycles can be designed by enhancing the processes of heating, recuperation, compression, and expansion. For a high-temperature heat source with a large specific heat capacity, the recompression configuration is suitable owing to its high efficiency and relatively simple structure. The split expansion configuration with reheating and intercooling is more suitable for heat sources with a small specific heat capacity. In addition, the CO2 power system combining the single-flow and split-flow cycles may provide a method to improve energy efficiency further, and fully utilize the advantages of both configurations. Furthermore, novel systems may be designed by combining the sCO2 cycle with the tCO2 cycle if the ambient temperature is low. The CO2 power cycle can also be integrated with refrigeration and heating devices to realize the comprehensive utilization of energy, which is of great significance for applications such as distributed energy systems.
Different sCO2 Brayton cycles have been investigated extensively for nuclear reactors, coal-fired plants, CSP, and high-temperature waste heat recovery. However, few investigations have focused on tCO2 cycles. More efforts are required to evaluate the feasibility and potential of different tCO2 Rankine cycles for low-grade heat sources, especially for small-scale applications. In practice, a comprehensive analysis of the CO2 power cycle, including an evaluation of its economic performance, is required. To accelerate the industrial application of CO2 power cycles, more efforts should be devoted to engineering activities, including component manufacturing, system seal, reliability and durability, system control, and optimization, in the future.
Statements
Author contributions
EW contributes to conceptualization, literature survey, paper drafting, and funding acquisition. NP is mainly responsible for the data curation and writing paper. MZ contributes to the paper modification, resources, visualization.
Funding
This research work was supported by the National Natural Science Foundation of China (Grant No. 51876009).
Conflict of interest
The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.
Publisher’s note
All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.
Abbreviations
CEPCI, chemical engineering plant cost index; CFC, chlorofluorocarbon; CHP, combine heat and power; CSP, concentrated solar power; GWP, global warming potential; HPT, high-pressure turbine; HTR, high-temperature recuperator; ICE, internal combustion engine; LNG, liquefied natural gas; LPT, low-pressure turbine; LTR, low-temperature recuperator; ODP, ozone depletion potential; ORC, organic Rankine cycle; PCHE, printed circuit heat exchanger; RC, Rankine cycle; sCO2, supercritical CO2 power cycle; TAC, turbine-alternator-compressor; tCO2, transcritical CO2 power cycle; VCC, vapor compression cycle.
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Summary
Keywords
Co2 power cycle, supercritical Brayton cycle, transcritical Rankine cycle, waste heat recovery, geothermal power plant, solar power generation
Citation
Wang E, Peng N and Zhang M (2021) System Design and Application of Supercritical and Transcritical CO2 Power Cycles: A Review. Front. Energy Res. 9:723875. doi: 10.3389/fenrg.2021.723875
Received
11 June 2021
Accepted
13 October 2021
Published
10 November 2021
Volume
9 - 2021
Edited by
Valerie Eveloy, Khalifa University, United Arab Emirates
Reviewed by
Silvia Lasala, Université de Lorraine, France
Fubin Yang, Beijing University of Technology, China
Stefano Mazzoni, Nanyang Technological University, Singapore
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*Correspondence: Enhua Wang, wangenhua@bit.edu.cn
This article was submitted to Process and Energy Systems Engineering, a section of the journal Frontiers in Energy Research
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