CFD investigation of body geometry effects on oil droplet-gas cyclone performance

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Abstract This study simulated gas flow in oil droplet-gas cyclones using the Reynolds stress turbulent model incorporated into the CFD code Ansys-Fluent. Five cyclone body designs, namely, cylindrical, square, octagonal, hexagonal, and inverted cone, were analyzed to determine their effect on gas flow patterns. The inverted cone geometry had a greater maximum tangential velocity, roughly 1.6 times the inlet gas velocity. In contrast, the square geometry had the lowest maximum axial velocity of 0.36 times the inlet velocity. The inverted cone cyclone showed the highest number of floating droplets, whereas the square cyclone yielded the least. Overall, the square shapes showed better performance than other shapes. The developed computational model accurately estimated droplet behavior, with its predictions closely matching the experimental data. Therefore, it is well-suited for simulating oil droplet motions in gas cyclones using CFD.

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Numerical investigation of effects of inner cone on flow field, performance and erosion rate of cyclone separators
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This study aims to determine the effect of a square cyclone body shape on the performance of a square cyclone separator. To achieve this goal, four square cyclone separators with square lengths 0, 1, 2, and 3 times the hydraulic diameter of the cyclone body were considered. The simulation of the gas-solid flow was carried out using the Euler-Lagrange approach, while the gas flow was modeled by Navier–Stokes equations and the Reynolds stress turbulent model (RSTM), and the injected solid particle was solved using the Newton equation. The pressure drop, separation efficiency, and flow pattern were investigated to evaluate the performance of square cyclone separators. The results revealed that the pressure drop and separation efficiency decreased as the relative square length increased. In the case with a lower relative square length, the vortex core penetration is less than that in the other cases, which leads to a decrease in the entrainment phenomena and separation efficiency enhancement. At an inlet velocity of 16 m/s, an increase in the relative square length from 0 to 3 reduced the pressure drop by approximately 35%. At an inlet velocity of 24 m/s and a particle diameter of 8 µm, with an increase in the relative square length from 0 to 3, the efficiency decreased from 88.7 to 77.4%.

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