2014
DOI: 10.1155/2014/619474
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Optimization of a Continuous Hybrid Impeller Mixer via Computational Fluid Dynamics

Abstract: This paper presents the preliminary steps required for conducting experiments to obtain the optimal operating conditions of a hybrid impeller mixer and to determine the residence time distribution (RTD) using computational fluid dynamics (CFD). In this paper, impeller speed and clearance parameters are examined. The hybrid impeller mixer consists of a single Rushton turbine mounted above a single pitched blade turbine (PBT). Four impeller speeds, 50, 100, 150, and 200 rpm, and four impeller clearances, 25, 50,… Show more

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Cited by 4 publications
(7 citation statements)
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“…The droplet is assumed to be an incompressible, viscous fluid. The governing equation can be expressed as [14] ∂u i ∂x i ¼ 0; ð5Þ and the Reynolds time-averaged N-S equation is shown as…”
Section: Numerical Simulationmentioning
confidence: 99%
“…The droplet is assumed to be an incompressible, viscous fluid. The governing equation can be expressed as [14] ∂u i ∂x i ¼ 0; ð5Þ and the Reynolds time-averaged N-S equation is shown as…”
Section: Numerical Simulationmentioning
confidence: 99%
“…The main concerns remain in determining the average residence time of the liquid phase and the variance of its distribution so as to represent the quality of its internal mixing performance and explain the difference from the continuous stirred tank reactor (CSTR). The main factors discussed are the physical properties of fluid , and the operation conditions, such as the type of impeller, the position of the impeller, the rotating speed, the relative position of the inlet and outlet, and the flow rate at the inlet. ,, Lipowska and Zhang et al showed that an increase in liquid viscosity could attenuate fluid mixing in the reactor. Samaras et al compared the performance of an axial-flow and two radial-flow impellers (Mixel TT and Rushton and NS turbines) on mixing in the reactor through a visual tracing experiment.…”
Section: Introductionmentioning
confidence: 99%
“…A deceleration-type duct is used. Most of the ducts in the IMP thruster are of the decelerating type, which can achieve the effect of deceleration and pressurization to delay the generation of cavitation and achieve the purpose of noise reduction [5]. According to Wang et al (2020), the IMP has several advantages compared to the conventional shaft-driven thruster, pod propulsor, and pump-jet propulsor [6]: (1) The IMP thruster has a high degree of integration, and the cabin reduces the complicated propulsion drive shaft system, auxiliary components, propulsion motors, and other equipment into a compact structure with a light weight.…”
Section: Introductionmentioning
confidence: 99%
“…The pump flow does not change much at different speeds when it has already maintained a certain speed. (5) The entire system works in fluid, which can solve the heat-dissipation problem of the motor by cooling the motor and the bearing. This can also reduce the energy consumed by these cooling systems.…”
Section: Introductionmentioning
confidence: 99%