DEVELOPMENT OF A SUPERCRITICAL CO2 BRAYTON ENERGY CONVERSION

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DEVELOPMENT OF A SUPERCRITICAL CO2 BRAYTON ENERGY CONVERSION ( development-supercritical-co2-brayton-energy-conversion )

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CHAetal., DevelopmentofaSupercriticalCO2BraytonEnergyConversionSystemCoupledwithaSodiumCooledFastReactor Table 3. Conceptual Design Parameters of the Compressor Diffuser loss External loss Average density Stage pressure difference Stage head Rotational speed Diameter Volume flow rate Specific speed Specific diameter Stage Table 4. Loss Model Summary of the Centrifugal Compressor Clearance loss Mixing loss Vaneless diffuser loss Disk friction loss Recirculation loss Leakage loss Jansen (1967) Jansen (1967) Unit kg/m3 MPa m rpm ft (ft3/s) - - Johnston and Dean (1966) Stanitz (1952) Daily and Nece (1960) Jansen (1967) Aungier (1955) Compressor 1 466.3 6.3 1377.8 3600 2.95 434.33 136.09 1.16 2 Fig. 4. Performance Characteristics of Compressor 1 for the Off-design-points Compressor 2 200.8 4.2 2119.3 3600 2.63 411.92 95.96 1.18 3 Internal loss Loss mechanism Incidence loss Blade loading loss Skin friction loss Loss model Conrad et.al (1980) Coppage et. al (1956) Fig. 5. Performance Characteristics of Compressor 2 for the Off-design-points flow rate were determined from the operation conditions; the maximum diameter and the head of the compressor were determined to maximize the efficiency, as seen in the diagram for the specific diameter and the specific speed. As a result of the iterative calculations, and based on the design parameters in Table 3, the stages of the two compressors (Compressor 1, Compressor 2) were determined as two and three, respectively. From Figure 3, the efficiency of the compressor was estimated during the process of the conceptual design to be more than 80% for the S-CO2 Brayton cycle coupled to the KALIMER-600. The diameter was estimated to be within 1 m for the two compressors. The performance analysis code, named COMP1D, for a centrifugal compressor for the S-CO2 cycle, was developed on the basis of the meanline analysis method, which is a one-dimensional analysis method. Since a sensitive loss model is required in order to include the effect of the impeller configuration and the flow path parameter, the loss model suggested by Oh was used to develop the code [11]. Performance analysis of the centrifugal compressor 1030 NUCLEAR ENGINEERING AND TECHNOLOGY, VOL.41 NO.8 OCTOBER 2009

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