基于响应面法的射流泵有限元仿真结构参数优化OA
Optimization of Structural Parameter for Jet Pump Based on Finite Element Simulation and Response Surface Methodology
为了增强气动力射流泵吸液性能、提高排水采气效率,以苏里格气田单管射流泵结构组件为研究对象,通过ANSYS建立仿真模型,以泵效作为射流泵性能的评价指标,对气动力射流泵结构参数进行分析.基于响应面法中的Box-Behnken Design设计试验方案,建立以喷嘴直径、喉嘴距、喉管直径及喉管长度为设计变量,以射流泵效率为优化目标的响应面模型,并通过对响应面模型进行泵效方差分析和结构参数相关性分析,确定了各结构参数对效率的影响程度依次为:喷嘴直径>喉管长度>喉管直径>喉嘴距;在优化范围内的最佳结构参数组合为:喷嘴直径dj 为3.3 mm、喉嘴距Lc 为4.3 mm、喉管直径dt为4.7 mm、喉管长度Lk 为25.76 mm.对比和分析仿真结果和试验结果,相对误差不大于 5%,验证了仿真模型和响应面模型的可靠性和准确性.
To enhance the suction performance of pneumatic jet pumps and improve drainage and gas production efficiency,we focuse on the single-tube jet pump structure in the Sulige Gas Field.Using ANSYS to establish a simulation model,we evaluate the pump's performance metrics by analyzing structural parameters.Based on the Box-Behnken Design in the response surface methodology,we develope a response surface model with nozzle diameter,nozzle-to-throat clearance,throat diameter and throat length as design variables,and jet pump efficiency as the optimization objective.Through variance analysis of pump efficiency and structural parameter correlation analysis on the response surface model,it is determined that the influence of each structural parameter on efficiency follows the order of:nozzle diameter>throat length>throat diameter>nozzle-to-throat clearance.The optimal parameter combination within the optimization range is determined as follows:nozzle diameter dj 3.3 mm,nozzle-to-throat clearance Lc 4.3 mm,throat diameter dt 4.7 mm and throat length Lk 25.76 mm.The simulation results and the experimental results are compared and analyzed,and the relative error is not more than 5%,which verifies the reliability and accuracy of the simulation model and the response surface model.
熊存燕
中海油田服务股份有限公司,天津 300459
机械制造
射流泵效率参数优化有限元仿真响应面法方差分析
jet pump efficiencyparameter optimizationfinite element simulationresponse surface methodologyvariance analysis
《液压与气动》 2026 (1)
86-95,10
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