Design method for s-CO2 gas turbine power plants

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Design method for s-CO2 gas turbine power plants ( design-method-s-co2-gas-turbine-power-plants )

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60 Components design system presented in Figure 2-23, corresponding to the minimum TIT for a pressure loss of 2%. However, the inlet pressure of CO2 is set to 50 bar and not to the value close to the critical pressure since the calculation procedure of ASPEN produces high deviations in the energy balance when working in this region. Both ASPEN and the present study consider similar calculation procedures since they divide the pipes in a specific number of sections and evalueate each section as an independent control volume. The number of elements for every single pipe has been set as 12. The results of the design are shown in Table 3-9. Table 3-9: Results of dimensioning calculations performed with ASPEN and the correlations for the dry cooler Tube side Inlet temperature Outlet temperature Inlet pressure Outlet pressure Pressure drop Tube length Air side Mass flow Inlet temperature Outlet temperature Pressure drop Heat transfer coefficient Fan power consumption Tubes and passes Number of tubes Number of rows Number of passes Other Bundle mass ◦C ◦C bar bar bar m kg/s ◦C ◦C Pa W/m2 K kW — — — tonne ASPEN Ferreira 113.08 113.08 31.57 31.24 50.00 50.00 49.84 49.90 0.16 0.10 9.85 7.78 346.51 346.51 15.00 15.00 49.99 50.17 47.00 66.62 — 77.19 21.56 22.17 4992 4992 8 8 1 1 19.89 15.26 Wang et.al. 113.08 31.24 50.00 49.93 0.07 5.01 346.51 15.00 50.20 171.29 326.70 56.99 4992 8 1 9.82 Both the correlations of Ferreira and Wang predict a lower tube length when compared with the one of ASPEN. However, Ferreira’s procedure gives a better result since the length of the tubes is closer to the one in the design done by ASPEN. The reason is the larger air side heat transfer coefficient given by the Wang correlations, leading to a lower tube length. As mentioned by these authors [8], their correlations are developed for smaller geometries, i.e., smaller tube diameter and pitch. This effect increases the air side heat transfer coefficient improving the performance of the heat exchanger and reducing its size. A schematic diagram of the cooler taken from ASPEN is presented in Figure 3-17. The only difference with the design developed in this work is the length of the tubes. J.S. Bahamonde Noriega Master of Science Thesis

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