2018
DOI: 10.3390/en11051048
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Design Method of Controllable Blade Angle and Orthogonal Optimization of Pressure Rise for a Multiphase Pump

Abstract: The hydraulic design method of controllable blade angle for rotodynamic multiphase pump with impeller and diffuser is proposed. The distribution of blade angle along the meridional streamline is governed by the normalized fourth-order and first-order polynomial function for impeller and diffuser, respectively. The orthogonal optimization method with five factors and four levels is employed by numerical simulation to optimize the geometry parameters, including the shroud angle at the leading and trailing edge β… Show more

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Cited by 68 publications
(26 citation statements)
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“…Thus, the SST k-w turbulence model can be used to obtain a very high accuracy and stability of the solution. In addition, it has been found that SST k-w turbulence model does a better job of predicting flow field in impeller than other turbulence models [37]; it is widely used in relevant studies on gas-liquid two-phase flow [38,39]. The pressure-based solver can provide Eulerian multiphase model, which is adopted in the numerical simulation.…”
Section: Methodsmentioning
confidence: 99%
“…Thus, the SST k-w turbulence model can be used to obtain a very high accuracy and stability of the solution. In addition, it has been found that SST k-w turbulence model does a better job of predicting flow field in impeller than other turbulence models [37]; it is widely used in relevant studies on gas-liquid two-phase flow [38,39]. The pressure-based solver can provide Eulerian multiphase model, which is adopted in the numerical simulation.…”
Section: Methodsmentioning
confidence: 99%
“…The convergence condition of the steady-state numerical calculation was set to an RMS value less than 10 −4 . Then, the steady-state simulation outcomes were obtained as the original value for the transient numerical calculation [19,20]. In accordance with the impeller rotation speed, the time step was determined to be Ti = 60/(3500 × 180) = 9.5238 × 10 −5 s. The different IGVFs were set at the inlet during the numerical simulations.…”
Section: Numerical Methods and Solution Settingsmentioning
confidence: 99%
“…The steady simulations were defined as a convergence when the value of root-mean-square residual was under 10 −5 . Unsteady simulations were then conducted with the results of the steady simulations [28][29][30]. Initially, the time step was determined in accordance with impeller rotation T i = 60/3600 = 8.6806 × 10 −5 s, and then the time step independence evaluation was carried out based on time steps of T i /96, T i /192, T i /384.…”
Section: Methodsmentioning
confidence: 99%