刷直流电机真空热特性的实验研究与数值分析

Tao Li, Tao Feng, Yaoting Wang, Xiangyang Xu
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引用次数: 0

摘要

刷直流(DC)电机具有多种特性,使其在太空飞行应用中非常有吸引力。考虑到航天任务对可靠性的高要求,对空间环境下刷直流电机的热特性和热失效进行了研究。利用电机热阻网络模型,确定了一种特殊的热测试方法,并结合热导率分析模型,通过逐项剥离获得热参数,构建了电机温度场。通过引入电弧放电因子来评估电腐蚀热耗,在转子失速、正转、单刷和多刷条件下,数值分析结果与试验结果吻合良好。分析和测试结果表明,连续运行110秒会导致电刷焊点熔化,电腐蚀热消耗是不可忽视的主要因素之一。真空应用的可靠性模型应在正负电极中至少有两个电刷的正常工作模式下建立。为了提高可靠性,提出了一种电机的密封充气结构,建立了无重力场的大曲率恒定连续介质流的热流协同仿真模型,得到了不同密封压力下的温度场和速度场。结果表明,单刷温度从真空中的204.5°C降至140°C以下,可以满足空间任务中刷电机高可靠性的长期连续工作要求。此外,研究发现,随着压力的降低,对流传热的影响逐渐减弱,温度逐渐升高并收敛于气体独特的热传导过程,而对流的影响可以忽略不计。随着压力的不断降低,密封气体从连续介质流演化为过渡自由分子流,气体的热传导效应再次减弱,直至接近单一固体传导过程。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental study and numerical analysis of vacuum thermal characteristics of brush DC motor

Brush direct current (DC) motors have several qualities that make them very attractive for space flight applications. Considering the high reliability requirements of aerospace missions, the thermal characteristics and thermal failure of the brush DC motor in the space environment were studied. Using a motor thermal resistance network model, a special thermal test method was determined and combined with a thermal conductivity analysis model, the thermal parameters were obtained via item-by-item stripping, and the motor temperature field was constructed. By introducing the arc discharge factor to evaluate the electric-corrosion heat consumption, the numerical analysis results were in good agreement with the test results under the conditions of stalled rotor, normal rotation, single brush, and multiple brushes. The analysis and test results show that continuous operation for 110 s will lead to melting of the brush solder joints, and electrical corrosion heat consumption is one of the main factors that cannot be ignored. The reliability model of vacuum applications should be established in the normal working mode of at least two brushes in both the positive and negative electrodes. To improve the reliability, a sealed air-filled structure of the motor was proposed, a heat-flow co-simulation model of a continuous medium flow with a large curvature and constant without a gravity field was established, and the temperature and velocity fields under different sealed pressures were obtained. The results show that the temperature of the single brush reduced to below 140 °C from 204.5 °C in vacuum, which can meet the long-term continuous working requirement of high reliability of brush motors in space missions. In addition, it was found that with the decrease in pressure, the effect of convective heat transfer gradually weakens, the temperature gradually increases and converges to the unique heat conduction process of the gas, while the effect of convection is negligible. As the pressure continues to decrease, the sealed gas evolves from continuous medium flow to transitional and free molecular flow, and the heat conduction effect of the gas weakens again until it approaches the singleness solid conduction process.

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