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基于风道系统模块化建模的翅片管蒸发器结构优化

Structure Optimization of Fin-and-Tube Evaporator Based on Modular Modeling of Air Duct System

  • 摘要: 为提高翅片管蒸发器空气侧换热效率,减小蒸发器阻力,以模块化建模计算方法与多变量线性回归算法相结合的方式分别构建蒸发器流量、压降与蒸发器结构参数映射关系模型。在映射关系模型的基础上,以最大化传热因子与最小化摩擦因子为优化目标,以蒸发器排间距与管间距为设计变量,使用NSGA-Ⅱ多目标算法寻优并获得最优解集。从最大化空气侧换热效率、最小化空气侧摩擦、损失少量换热效率换取摩擦显著降低和折中考虑换热效率与摩擦四个角度进一步分析最优解集,获取四种情况下最优解并进行验证。结果表明:优化结果与仿真结果误差不超过5.6%,且相比于原始尺寸参数蒸发器换热效率与阻力特性均有不同程度提升。

     

    Abstract: To improve the air-side heat transfer efficiency and reduce the resistance of fin-and-tube evaporator, this paper combines the method for modular modeling calculation and the algorithm for linear regression with multiple variables to construct the mapping relationship models of flow rate, pressure drop and the structure parameters of the evaporator. And based on the mapping relationship model, the multi-objective optimization is aimed at achieving maximum the Colburn factor and minimum friction factor by the NSGA-Ⅱ algorithm with regards to design variables, the row spacing and tube spacing of evaporators. According to this, the set of multi-objective optimization is analyzed and verified by the following four aspects: maximizing the air-side heat transfer efficiency, minimizing the air-side friction, significantly reducing the friction based on a small loss of heat transfer efficiency, and compromising the heat transfer efficiency and friction. The error between the final optimization results and the simulation results is less than 5.6%, and compared to the initial structure parameters of the evaporator, the heat transfer efficiency and resistance characteristics have been improved to varying degrees.

     

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