近地轨道用平板太阳能热电发电板的制造

F. K. Eggleston, N. Fuschillo
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引用次数: 4

摘要

针对平板热电发电机单元偶(约1英寸乘1英寸)和面板(约3英寸乘3英寸),开发了一种实用的热机械结构设计。叙述了制造这些太阳能转换装置所使用的技术。由此产生的单元耦合器提供3瓦/平方英尺,耦合器的重量因子为30瓦/磅,面板形式的重量因子为15瓦/磅。稳态和热循环寿命试验表明,在2000次循环中,输出衰减小于10%。这些结果为低成本的空间电力系统提供了希望,该系统具有特殊的适应性,可以适应不适合光伏电池的任务。描述了9个单元电池的3 × 3英寸面板的制造,提供15瓦/磅。
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Fabrication of Flat Plate Solar Thermoelectric Generator Panels for Near-Earth Orbits
A practical thermomechanical configurational design was developed for flat plate thermoelectric generator unit couples (approximately 1 inch by 1 inch) and panels (approximately 3 inches by 3 inches). An account of the techniques used in fabricating these solar energy conversion devices is given. Resulting unit couples provide 3 watts/ft2 with a weight factor of 30 watts/lb for the couple and 15 watts/lb for the panel form. Steady-state and thermal cycle life tests indicate an output degradation of less than 10% in 2000 cycles. These results offer promise of lower cost space power systems with special adaptability to missions not suited to photovoltaic cells. The fabrication of 3-by 3-inch panels of nine unit cells giving 15 watts/lb is described.
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