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林高伟, 徐毓贤, 刘雪涛, 等. 基于CFD的雷蒙磨粉机分级机涡轮优化设计J. 桂林电子科技大学学报, 2025, 45(2): 182-188. DOI: 10.16725/j.1673-808X.2022201
引用本文: 林高伟, 徐毓贤, 刘雪涛, 等. 基于CFD的雷蒙磨粉机分级机涡轮优化设计J. 桂林电子科技大学学报, 2025, 45(2): 182-188. DOI: 10.16725/j.1673-808X.2022201
LIN Gaowei, XU Yuxian, LIU Xuetao, et al. Turbine optimization design of Raymond mill classifier based on CFDJ. Journal of Guilin University of Electronic Technology, 2025, 45(2): 182-188. DOI: 10.16725/j.1673-808X.2022201
Citation: LIN Gaowei, XU Yuxian, LIU Xuetao, et al. Turbine optimization design of Raymond mill classifier based on CFDJ. Journal of Guilin University of Electronic Technology, 2025, 45(2): 182-188. DOI: 10.16725/j.1673-808X.2022201

基于CFD的雷蒙磨粉机分级机涡轮优化设计

Turbine optimization design of Raymond mill classifier based on CFD

  • 摘要: 雷蒙磨粉机在建筑材料生产加工过程中应用广泛,但其分级机涡轮存在气流运行不通畅问题,严重影响工作效率。针对这一问题,首先建立模型并对其进行流体仿真分析,在Solidworks中对雷蒙磨粉机分级机涡轮进行参数化建模,通过有限元软件对其进行气动分析,得到原气动阻力系数;然后通过Isight软件联合Solidworks、Icem以及Fluent对雷蒙磨粉机分级机涡轮的结构进行集成仿真优化,选择4个设计变量在Isight中进行DOE试验,并建立了二阶响应面近似模型,再对优化模型进行误差分析,得到拟合优度为0.98,从而确定了此模型的可行性;最后结合序列二次规划法(NLPQL),并以最小气动阻力系数为目标函数,对结构参数进行优化计算,结果表明雷蒙磨粉机的Z轴方向气动阻力系数由优化前的21.44减少到优化后的18.97,Z轴方向气动阻力系数减少了11.52%,效果较好。

     

    Abstract: Raymond mill is widely used in the production and processing of building materials, but the turbine of its classifier has the problem of unsmooth airflow, which seriously affects its working efficiency. In order to solve this problem. Firstly, the model was established and the fluid simulation analysis was carried out. In Solidworks, the parametric modeling of the Turbine of Raymond mill classifier was carried out. This model was mainly based on the top-down design of Solidworks 2020 to complete the correlation between parameters. Then the original aerodynamic drag coefficient was obtained by aerodynamic analysis with finite element software. Then, Isight software combined with Solidworks, Icem and Fluent was used to optimize the turbine structure of Raymond mill classifier. Four design variables were selected to conduct DOE test design in Isight, and a second-order response surface approximation model was established to analyze the error of the optimization model, and the goodness of fit is 0.98, so as to confirm the feasibility of the model. Finally, combined with sequential quadratic programming (NLPQL) and the minimum aerodynamic drag coefficient as the objective function, the structural parameters were optimized and calculated. Finally, the aerodynamic resistance coefficient in Z-axis direction of Raymond mill is reduced from 21.44 before optimization to 18.97 after optimization, and the aerodynamic resistance coefficient in Z-axis direction is reduced by 11.52%, showing a good effect.

     

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