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中国物理学会期刊

星载电子器件温控的系统多尺度分析

CSTR: 32037.14.aps.73.20240685

System multi-scale analysis of temperature control for spaceborne electronic devices

CSTR: 32037.14.aps.73.20240685
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  • 为提高星载电子器件热分析的模拟分辨率和精度以及被动热控装置的控温效果, 本文建立系统多尺度模型获得不同尺度下卫星内部电子器件的温度场和热流信息. 结果表明: 系统多尺度模型在系统级尺度模拟精度与实际模型相对误差小于9%, 并且可消耗较少的计算资源获得器件级尺度芯片微小结构的热信息. 系统级模型可从宏观尺度评估星载被动热控材料的控温隔热性能, 采用复合相变隔热材料可将载荷舱室温度波动幅值降至2.43 K, 相比平台舱室温度波动幅值降低约69.43%, 通过复合相变隔热材料隔热后的温度波动信号呈现向高频域部分转移的特征. 基于多元回归分析选定需要进行重点隔热控温的舱室后, 采用器件级简化模型得到不同热控装置布局下的温度场信息形成训练数据集, 采用神经网络遗传算法在器件尺度预测被动热控装置的最佳安装位置, 并得到减小器件最大温度波动的热控布局方案, 最大温度波动降低2.74 K.

     

    To improve the simulation resolution and accuracy in thermal analysis of spaceborne electronic devices and the temperature control performance of passive thermal control devices, a system multi-scale model is established, thereby obtaining the temperature field and heat flux of electronic devices inside the satellite on different scales as illustrated in the below figure. The temperature fluctuation mechanism inside the satellite is analyzed on different physical scales. The thermal analysis resolution of spaceborne electronic equipment is improved, and a method to reduce the power fluctuation of spaceborne equipment is proposed based on the results of system multi-scale thermal analysis.
    The results indicate that the accuracy deviation between the multi-scale model of the system and the actual model is less than 9%. However, the system multi-scale model saves 99.67% of the mesh generation time, which greatly improves the computation efficiency. The system multi-scale model can capture the thermal information about device-level chip microstructures at a lower computational cost. The system-level model can evaluate the temperature control and insulation performance of passive thermal control materials on a macroscale. The temperature fluctuation amplitude of the platform compartment is 7.95 K, while the temperature fluctuation amplitude of the load compartment decreases to 2.43 K after the temperature of the composite phase change insulation material has been controlled, which is 69.43% lower than that of the platform compartment. Compared with traditional vacuum insulation panels, the composite phase change materials are very superior in controlling the temperature of the chamber and suppressing temperature fluctuations. The temperature fluctuation signal after being insulated by the composite phase change insulation materials shows a characteristic of shifting to the high-frequency domain. After selecting the cabins that require key insulation and temperature control through multiple regression analysis, a simplified model at device level is employed to obtain temperature fields under different thermal control device layouts as a training dataset. A neural network genetic algorithm is used to predict the optimal installation position of passive thermal control device on the device scale and a thermal control layout scheme is obtained, which reduces the maximum temperature fluctuation of the device by 2.74 K. If the temperature uniformity coefficient is taken as the optimization goal, the temperature of each device on PCB board can be reduced to 14.39% of the average temperature of all devices through optimizations.

     

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