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SMALL-SCALE RADIAL INFLOW TURBINE FOR WHR ORC

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SMALL-SCALE RADIAL INFLOW TURBINE FOR WHR ORC ( small-scale-radial-inflow-turbine-for-whr-orc )

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CHAPTER 5: Mean-line Modelling and Optimization of Organic RIT and Integration with Cycle Analysis Programme parameters at the rotor outlet (St,5, Tt,5, ρt,5, Pt,5, Pt,5,rel, ht,5,rel ,T5, h5, ρ5) were determined using the isentropic expansion state point (h5s, S5s=S1), Ξ”hactual and (C5,W5). The rotor exit flow area (A5) and the rotor exit tip radius (r5,tip) were obtained as below using the known r5hub/r4 ratio given in Table 5-3. 𝐴5 = π‘Ÿ 5,𝑑𝑖𝑝 π‘šΜ‡ π’˜π’‡ Equation 5-19 πœ‘π‘ˆ4𝜌5(1βˆ’π΅πΎ) = √𝐴5 + π‘Ÿ2 Equation 5-20 πœ‹ 5,h𝑒𝑏 Same value for BK was used similar to chapter three and the same correlation was employed for specifying Zrotor shown in Equation 3-26. In order to determine the rotor blade inlet angle (Ξ²4,blade) the below equations were used (Aungier 2006). πœ… = 1 βˆ’ π‘π‘Ÿπ‘œπ‘‘π‘œπ‘Ÿ 𝑑4 2πœ‹π‘Ÿ cos𝛽 Equation 5-21 Equation 5-22 4 𝐢 = (1 βˆ’ √cos 𝛽4,π‘π‘™π‘Žπ‘‘π‘’) (π‘ˆ πœƒ,4 π‘π‘Ÿπ‘œπ‘‘π‘œπ‘Ÿ0.7 4 4,π‘π‘™π‘Žπ‘‘π‘’ βˆ’ 𝐢 π‘š,4 tan 𝛽4,π‘π‘™π‘Žπ‘‘π‘’) πœ… Where t4 is the rotor blade inlet thickness equal to 0.04r4 according to (Aungier 2006). EES can iteratively solve the two above explicit equations for Ξ²4,blade. 5.4.3. Nozzle modelling Modelling of nozzle is similar to section 3.5.3 with the only difference that the ratio of nozzle inlet to exit (r2/r3) was taken as a free parameter shown in Table 5-3. In addition, instead of using the cambered vanes shown in Figure 3-8, un-cambered nozzle vane geometry was created as the nozzle ring was located after the volute. 5.4.4. Volute modelling To transfer the fluid uniformly around the periphery of the nozzle ring, the ratio of the volute inlet area to inlet radius (A1/r1) should be a linear function of the polar angle. Assuming circular cross section for the volute shown in Figure 5-4, key geometry and 167 | P a g e

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