首页|多室连续混合设备桨叶设计参数优化

多室连续混合设备桨叶设计参数优化

Optimized design of blade parameters of multi-chamber continuous mixing equipment

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为优化多室连续混合设备的设计参数,开展多室连续混合设备桨叶多目标优化研究.以混合室单位体积功耗和混合室轴截面有效混合面积为目标函数,峰值剪切应力为约束变量,建立了基于径向基函数的多目标优化模型,采用正交试验设计和遗传算法对桨叶进行了参数优化,并对优化结果进行了CFD仿真和试验验证.结果表明,多室连续混合设备特性参量的显著影响因素为桨叶外径、桨叶-壁面间隙以及桨叶转速.相对于初始设计,优化后单位体积功耗降低了14.90%,混合室轴截面有效混合面积增加了 4.10%,二者乘积降低了 11.47%,峰值剪切应力降低了 21.28%,在混合能力降低较少的情况下安全性获得了较大的提升,证明了基于径向基函数的多目标遗传算法在多室连续混合设备性能优化上的可行性.
In order to optimize the design parameters of multi-chamber continuous mixing equipment,the multi-objective optimi-zation research of propeller blades of multi-chamber continuous mixing equipment was carried out.A multi-objective optimization model based on radial basis function was established by taking the power consumption per unit volume of the mixing chamber and the effective mixing area of the shaft section of the mixing chamber as the objective function and the peak shear stress as the limiting variable.The orthogonal experimental design and genetic algorithm were used to optimize the parameters of the impeller,and the opti-mization results were verified by CFD simulation and experiment.The results show that the significant influencing factors of the char-acteristic parameters of multi-chamber continuous mixing equipment are the outer diameter of the blade,the blade-wall gap and the rotate speed.Compared with the initial design,the power consumption per unit volume is reduced by 14.90%,the effective mixing ar-ea of the shaft section of the mixing chamber is increased by 4.10%,the product of the two is reduced by 11.47%,and the peak shear stress is reduced by 21.28%.The safety is greatly improved with less reduction in mixing capacity,which proves the feasibility of multi-objective genetic algorithm based on radial basis function in the performance optimization of multi-chamber continuous mix-ing equipment.

continuous mixingbladeorthogonal experimental designmulti-objective optimizationradial basis functions

阮班铖、金文强、魏宗亮、谢中元、陈松

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西安近代化学研究所,西安 710065

中国兵器工业集团航空弹药研究院有限公司,哈尔滨 150030

连续混合 桨叶 正交试验设计 多目标优化 径向基函数

2024

固体火箭技术
中国航天科技集团公司第四研究院 中国宇航学会固体推进专业委员会

固体火箭技术

CSTPCD北大核心
影响因子:0.461
ISSN:1006-2793
年,卷(期):2024.47(1)
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