Analysis of a Radial Outflow Turbine for Organic Rankine Cycles

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Analysis of a Radial Outflow Turbine for Organic Rankine Cycles ( analysis-radial-outflow-turbine-organic-rankine-cycles )

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Energies 2020, 13, 2118 17 of 19 7. Conclusions In this study, a preliminary design algorithm for ORC radial outflow turbines was presented. This algorithm uses models of axial turbines due to the absence of enthalpy loss models and deviation angle models for radial outflow turbines. As a result of evaluating the algorithm through CFD, the algorithm showed an accuracy of about 95% based on the turbine power. That is, it was realized that models derived from the axial turbine are also effective in the preliminary design of the radial outflow turbine. Due to the high accuracy of the algorithm developed in this study, the designed turbine could satisfy the target power (400.0 kW) and total-to-static efficiency (85.0%) by fine-tuning the blade angle of the nozzle exit. In addition, the off-design performance for various operation conditions was examined in this study. Through off-design analysis, it is considered that the appropriate ranges of velocity ratio, loading coefficient, and flow coefficient that can expect high efficiency in a radial outflow turbine are 0.57–0.70, 0.85–1.30, and 0.34–0.41, respectively. The findings of this study are expected to be a useful reference in the design of radial outflow turbines for organic Rankine cycles. Nomenclature 𝑏𝑏 Radial chord 𝑃𝑃 𝐢𝐢 Absolute velocity 𝑃𝑃𝑅𝑅 𝑐𝑐 True chord π‘Ÿπ‘Ÿ Pressure Pressure ratio Radius Reynolds number Entropy, Pitch Temperature Blade thickness Temperature ratio Peripheral velocity Relative velocity Turbine power Dynamic viscosity Velocity ratio Enthalpy loss coefficient Density Flow coefficient Loading coefficient Angular velocity 𝐢𝐢0 Spouting velocity 𝑅𝑅𝑅𝑅 𝐷𝐷h Hydraulic diameter 𝑠𝑠 𝐻𝐻 Height 𝑇𝑇 h Enthalpy 𝑑𝑑 𝑠𝑠 Incidence angle 𝑇𝑇𝑅𝑅 𝑀𝑀 Mach number π‘ˆπ‘ˆ π‘šπ‘šΜ‡ Mass flow rate π‘Šπ‘Š Μ‡ 𝑁𝑁 Number of blades π‘Šπ‘Š 𝑐𝑐 Throat Greeks 𝛼𝛼 Absolute flow angle πœ‡πœ‡ 𝛽𝛽 Relative flow angle 𝜈𝜈 𝛽𝛽𝑔𝑔 Gauging angle πœ‰πœ‰ 𝛿𝛿 Deviation angle 𝜌𝜌 πœ€πœ€ Deflection angle πœ™πœ™ 𝜁𝜁 Loss coefficient πœ“πœ“ πœ‚πœ‚ Efficiency πœ”πœ” 0 Total state 00 Total state at station 0 Subscripts π‘šπ‘šπ‘ π‘ π‘ π‘  𝑁𝑁 Nozzle 𝑅𝑅 Rotor 1 Nozzle inlet 2 Nozzle exit & Rotor inlet 3 Rotor exit 𝑏𝑏 Blade Minimum 𝑑𝑑𝑅𝑅𝑠𝑠𝑠𝑠𝑑𝑑𝑠𝑠 Design point π‘šπ‘š Meridional component 𝑠𝑠 Isentropic 𝑑𝑑𝑠𝑠 Total to static 𝑑𝑑𝑑𝑑 Total to total π‘šπ‘šπ‘šπ‘šπ‘šπ‘š Maximum πœƒπœƒ Tangential component π‘Ÿπ‘Ÿ Relative

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