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Development of Thermophotovoltaic Devices Optimized for High Temperature Operation

机译:高温操作优化的蒸发器装置的研制

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The recent interest in thermophotovoltaics (TPV) for space power applications has necessitated consideration of new device designs that are optimized for operation at elevated temperatures in order to be compatible with practical space-platform power systems. Photovoltaic device performance degrades as operating temperature is increased due to increasing dark current density (Jo). A cooling system is therefore required to maintain a low cell temperature with respect to the emitter (~1300 K). However, the cold-side cooling capacity is directly related to the temperature, size and mass of a passive radiator. Therefore, since a high power to weight ratio is a critical factor for spacecraft power system design, the ability to realize devices capable of improved power density at elevated temperatures is critical to minimize the mass of space TPV systems. A simple model has been developed to estimate the effect of temperature on device electrical properties. Design parameters under investigation are the modification of bandgap, layer thickness and doping levels in the active device junction. Preliminary results of the modeling effort suggest that the optimum design for a device operated at room temperature differs from that of a device operated at elevated temperature.
机译:近期对空间电力应用的蒸发器(TPV)的兴趣已经需要考虑在高温下针对操作进行优化的新设备设计,以便与实用的空间平台电力系统兼容。由于暗电流密度增加(jo),光伏器件性能降低,因为较大的暗电流密度(jo)增加。因此,需要冷却系统以相对于发射器(〜1300k)保持低电平的细胞温度。然而,冷侧冷却能力与无源散热器的温度,尺寸和质量直接相关。因此,由于重量比的高功率是航天器电力系统设计的关键因素,因此实现能够改善电力密度在升高的温度下能够改善功率密度的能力,这对于最小化空间TPV系统的质量是至关重要的。已经开发了一种简单的模型来估计温度对器件电性能的影响。正在调查的设计参数是有源器件结的带隙,层厚度和掺杂水平的改变。建模工作的初步结果表明,在室温下操作的装置的最佳设计与在升高温度下操作的装置的最佳设计不同。

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