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Automotive Radial Turbine Expander Design WHR

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Automotive Radial Turbine Expander Design WHR ( automotive-radial-turbine-expander-design-whr )

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116 reduction of the total pressure from the stator trailing edge and rotor leading edge is 1.45%, which is sufficiently small to validate a constant total pressure in the interspace. Watanabe et al. [243]proposed a correlation to estimate a suitable clearance gap between the stator exit and the rotor inlet, as shown in equation (β€Ž5-34). The maximum turbine efficiency can be achieved by placing a value of 2 for π‘˜. π‘Ÿ βˆ’ π‘Ÿ = π‘˜ 𝑏 𝑐 π‘œ 𝑠 𝛼 3 + 𝛼 4 , ( β€Ž5 - 3 4 ) 2 where 𝑏3 is the stator blade height calculated using equation (β€Ž5-35). πœ€π‘₯ and πœ€π‘Ÿare the axialand radial tip clearances, as shown in Figure β€Ž4-2, and they are calculated using equation (β€Ž5-36)[234]. 343 𝑏3 = 𝑏4 + πœ€π‘₯ πœ€π‘₯ = πœ€π‘Ÿ =0.04𝑏5 5.3.4 Stator Modelling (β€Ž5-35) (β€Ž5-36) To reduce incidence loss, the nozzle vanes must be set at an appropriate blade angle to enable a smooth swirl flow at the rotor leading edge. The design procedure of the nozzle vanes are performed iteratively, as shown in the flowcharts inFigure β€Ž5-3 and Figure β€Ž5-4. Li et al. [244] stated that the conservation of angular momentum can be applied in the vaneless space because the swirl coefficient (SC) between the stator exit and the rotor inlet is close to unity. Therefore, the tangential component of the velocity at the stator exit πΆπœƒ3 can be calculated, as shown in equation(β€Ž5-37). πΆβˆ™π‘Ÿ πΆπœƒ3=πœƒ4 4 To construct the velocity triangle at the stator exit, the absolute velocity 𝐢3 is calculated iteratively with a first assumption of 𝐢3 = πΆπœƒ3. Subsequently, the static enthalpy 𝑕3 is calculated from the total enthalpy and the kinetic energy, as shown in equation(β€Ž5-38). π‘Ÿ 3 (β€Ž5-37)

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