Based on the first and second laws of thermodynamics, parameters of the supercritical carbon dioxide (S-CO₂) recompression cycle, recompression reheat cycle, partial cooling cycle, partial cooling reheat cycle coal-fired power generation system were calculated and analyzed by using MATLAB software. Then, the impact of shunt coefficient, outlet and inlet pressure of the main compressor on the system circulation efficiency, equipment and exergy efficiency of the system were discussed respectively, and the four types of circulation systems were compared and analyzed. The results show that the cycle efficiency varies with the same parameters under different cycle layout or the same cycle layout and different operating parameters. There is a shunt coefficient for exergy efficiency and exergy efficiency to reach an optimal value. There is a coupling relationship between the influence of outlet and inlet pressure of the main compressor and the shunt coefficient on the circulation efficiency. For different parameter changes, exergy efficiency of system is mainly affected by exergy efficiency of different equipment. Reheat can increase circulation efficiency and exergy efficiency of the system, while some cooling cycles are relatively less sensitive to parameter changes.

In order to improve the operation flexibility of coal-fired power units, a thermal system of coal-fired power system coupled with supercritical carbon dioxide (S-CO₂) energy storage cycle is proposed, and the effect of operation parameters on the system irreversible loss is investigated by thermodynamic exergy analysis. The results show that, the energy storage efficiency of the system can reach 56.14%, and the S-CO₂ flow rate and the S-CO₂ compressor/turbine pressure ratio have a greater influence on the system exergy efficiency. With the increase of S-CO₂ flow rate from 50 kg/s to 70 kg/s, the exergy efficiency of the system increases from 44.0% to 61.0%. With the increase of compressor/turbine pressure ratio from 3.0 to 6.0, the exergy efficiency of the system increases from 27.5% to 52.5%. The method proposed provides a theoretical reference for improving the coal-fired power unit operation flexibility, and provides ideas for large-scale grid connection of renewable energy.

A high-parameter gas turbine and supercritical carbon dioxide (S-CO₂) combined cycle model was constructed, and thermal performance analysis was carried out. The top cycle uses a high-parameter gas turbine with a combustion chamber exhaust temperature of 1 800 ℃, and the bottom cycle adopts S-CO₂ Rankine double turbine cycle, while using three-stage flue gas heating and two-stage turbine exhaust gas recovery. The parameters and thermal performance under the optimized combined cycle operating conditions are obtained by the penalty function method. The influences of the main parameters of the high-parameter gas turbine top cycle and S-CO₂ Rankine bottom cycle on the combined cycle performance is analyzed. The results show that the combined cycle thermal efficiency can reach 68.61% at the gas turbine pressure ratio of 35.5 and the combustion chamber outlet temperature of 1 800 ℃, and the efficiency of the combined cycle of the gas turbine and S-CO₂ is 2.3 percentage points higher than that of the combined cycle of the gas turbine and steam.

The supercritical carbon dioxide cycle has many advantages, such as high cycle efficiency, small equipment size, convenient transportation and installation, and easy to reach the critical point. Considering the huge cold energy of LNG, it can not only be used as coolant in the combined cycle system, but also the natural gas after heat transfer can be used as fuel input in the combined cycle, and the rest can be supplied to urban users. A gas turbine/supercritical carbon dioxide combined cycle system based on the utilization of LNG cold energy is proposed in this paper. Select the appropriate cost formula to calculate and analyze the investment cost, operating income and recovery cycle of the circulating power generation system in detail. The influence of some key parameters (such as maximum temperature, maximum pressure, minimum temperature, minimum pressure and shunt ratio) on the power generation characteristics and economy of the supercritical carbon dioxide cycle in the combined cycle system was studied. The results show that with the increase of each single parameter, the cost of equipment investment will first increase and then decrease, but the effect of power generation on income is dominant. Taking the yield as the measurement standard, the higher the maximum temperature, the better, the lower the minimum temperature, the better. Under other parameters, there are optimal values to maximize the yield.The key parameters were optimized by genetic algorithm to maximize the cumulative income. After optimization, the recovery cycle was 5.86 years, and the cumulative income (20 years) was 2.287 billion yuan.

Aiming at the problem of waste heat utilization of gas turbine, the technologies of intermediate cooling, intermediate reheating and split flow recompression were introduced into the supercritical carbon dioxide (S-CO₂) power cycle with heat recovery and six cycle schemes were established. Taking the cycle efficiency and the cycle net output power of the S-CO₂ cycle as the optimization objectives, the genetic algorithm was used to optimize the parameters of each scheme, and the earnings of optimization results were compared. The results show that the cycle efficiency can be improved in varying degrees by introducing one intermediate cooling, one intermediate reheat and one split flow recompression when the optimization goal is to maximize the cycle efficiency. The cycle efficiency of the sixth scheme that introduces one split flow recompression and one intermediate reheat is the highest, which reaches 43.29%. When the optimization goal is to maximize the net cycle output work, the introduction of primary intermediate cooling can increase the net output power, the introduction of primary intermediate reheating can reduce the net output power of the power cycle, and the one split recompression degenerates into no split scheme. The second scheme that introduces primary intermediate cooling has the largest net output power reaching 82 620.02 kW. When the cycle net output work is taken as the optimization objective, the economy of the six schemes is more advantageous because the waste heat utilization efficiency of gas turbine smoke exhaust is higher. The second scheme has the largest operating earnings in 20 years, which is RMB 5.065 billion.

Centrifugal compressor is one of the key components in supercritical carbon dioxide (S-CO₂) cycle system, which plays a decisive role in the efficiency and stable operation of the system. Different from the traditional air compressor, the unique physical properties of S-CO₂ working medium make the internal flow field of the compressor more complex. The loss model established based on the physical characteristics of air also needs to be modified specifically to meet the performance prediction requirements of S-CO₂ centrifugal compressor. Therefore, numerical simulation is needed to investigate the internal flow field characteristics of the compressor, so as to improve the compressor performance prediction method accordingly. Firstly, one-dimensional aerodynamic parameters of the compressor were designed, and a three-dimensional model was established based on the one-dimensional design parameters to analyze the characteristics of the internal flow field of the compressor. It was found that the shunt blade had a great influence on the internal flow field, and changes in the internal flow field of the impeller under varying working conditions would also cause changes in the outlet flow Angle. Based on this, The sliding factor and the calculated blade number of the compressor under off-design conditions were corrected, and the surface friction coefficient was improved to predict the performance of the compressor under off-design conditions. The numerical simulation results show that the prediction error of the improved model is significantly reduced, and the average efficiency error decreases from 2.03% to 0.16% under off-design conditions.

As the core equipment of supercritical carbon dioxide (S-CO₂) Brayton cycle, there is a lack of reliable evaluation and test verification of the overall performance. An in-depth simulation and performance analysis of one axial turbine are carried out, focusing on the impact of inlet and exhaust housings with experiment results for different operating conditions. The results show that the numerical calculation method and model are able to evaluate the performance at different load conditions more accurately. Compared with the test results, the maximum efficiency error is 1.77 percentage point and the flow rate error remains within 5.6%. The crown pattern can reduce leakage and mixing losses, and increase efficiency by 1.4 percentage point compared to the common top clearance pattern. Simulation results show that the efficiency of turbine unit is reduced compared to turbine stage, with a maximum reduction by 2.9 percentage point. The flow loss of inlet and exhaust housings is the main reason for the reduction. The research results can provide technical support for the design and performance simulation of S-CO₂ axial turbines.

A cooling system was designed for a supercritical carbon dioxide (S-CO₂) axial turbine. The dry gas seal, shaft and casing were cooled by extracting the low temperature S-CO₂ in the pipeline behind the compressor to ensure that the dry gas seal operating temperature was below 200 ℃. The flow and heat transfer characteristics of the cooling system were analyzed using the coupled heat transfer method, and the temperature distributions of solid domains such dry gas seal, shaft and casing of different cooling schemes were compared. The research shows that the temperature drop of the shaft reaches 220.3 ℃ when the_shaft cooling scheme is adopted, and the maximum temperature of the dry gas seal is 229.1 ℃. Further introduction of S-CO₂ with lower temperature and larger flow rate to cool the casing can inhibit the heating effect of the high temperature mainstream at the turbine inlet. The temperature drop of the shaft increases to 244.1 ℃, and the maximum temperature of the dry gas seal decreases to 181.2 ℃. Meanwhile, the reasonable temperature gradient of the cooled domains such as the dry gas seal, shaft and casing is achieved. The cooling system designed in this paper provides a solution for the safe and reliable operation of S-CO₂ axial turbines.

To ensure the safe and reliable operation of supercritical carbon dioxide (S-CO₂) power plant over a long period of time, referred to the material commonly used in traditional steam boiler, the material of S-CO₂ boiler is selected fromhigh temperature strength and corrosion characteristics. When CO₂ flows through the boiler, the temperature of CO₂ is high, the temperature difference between CO₂ and tube wall temperature is large, over the 30~50 ℃ of steam boiler. Then the grade of the heat-resistant steel has to be upgraded. However, requirements and methods for the material selection for steam boiler cannot be directly used for S-CO₂ boiler. The feasibility of heat-resistant steels such as T23, T91,T92, TP347HFG and Super304H used in S-CO₂ boilers is explored from using maturity and economic performance. The results show that for cooling wall, T91 could be selected at certain tube structure, but 12Cr1MoVG, T21 and T23 et al used in steam boiler could not be selected. For superheater, only austenitic steel TP347HFG and Super304H meet the material selection requirements at certain tube structure.

Aiming to the performance analysis of boiler with supercritical carbon dioxide (S-CO₂) cycle, the boiler performance evaluation index system is built by taking the gas-fired boiler used in the 5 MW S-CO₂ Brayton cycle pilot unit at Xi'an Thermal Power Research Institute Co., Ltd. as the research object. The core performance indexes of S-CO₂ boiler include the fuel efficiency of boiler, the ratio of heat absorption over the input heat for each heat exchanger, the performance of air preheater, the pressure drop of working fluid system, the NO_x emission concentration, and others. The fuel consumption and excess air coefficient are calculated via the measurement of oxygen concentration. Meanwhile, the calculation method of heat loss due to exhaust gas is improved. The ratio of heat absorption over the input heat for each heat exchanger is introduced, which shows the contribution of each heat exchanger on heat absorption process. Finally, the calculation process is integrated becoming to an executable program, and it is applied in the running and monitoring procedures. An operating case showed that, for the research object, the actual condition is basically the same as that of the design parameters. The finally calculated boiler fuel efficiency is 92.05% without correction and 93.79% with correction, the later is similar as the designed value (93.53%).