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基于响应曲面法的微型核素恒温器翅片优化设计

Optimal Design of Micro-nuclide Thermostat Fin Based on Response Surface Method

  • 摘要: 为提高恒温器散热性能,以微型核素恒温器散热翅片为研究对象,根据Box-Behnken响应曲面法设计恒温器翅片响应曲面分析实验,模拟分析翅片不同结构参数组合下恒温器的散热性能,探究散热性能最佳时的翅片结构参数。结果表明:不同翅片结构参数组合下恒温器的散热性能不同,散热性能最佳的翅片厚度1.058 mm、翅片间距2.014 mm、翅片长度43.996 mm、翅片与内壁距离3.850 mm;优化后恒温器最高散热温度为77.37℃,与原恒温器相比,最高散热温度下降了1.09℃,散热性能得到了提高。

     

    Abstract: In order to improve the heat dissipation performance of the thermostat, the heat dissipation fin of the micronuclide thermostat was taken as the research object, the response surface analysis experiment of the thermostat fin was designed according to the Box-Behnken response surface method. The heat dissipation performance of the thermostat under different combinations of fin structure parameters were simulated and analyzed, and the fin structure parameters with the best heat dissipation performance was explored. The results show that the heat dissipation performance of the thermostat is different under the different structure parameters. The best fin thickness is 1.058 mm, the spacing is 2.014 mm, the length is 43.996 mm, and the distance between the fin and the inner wall is 3.850 mm. After optimization, the maximum heat dissipation temperature of the thermostat is 77.37℃. Compared with the original thermostat, the maximum heat dissipation temperature decreases by 1.09℃, and the heat dissipation performance is improved.

     

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