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Scale limitations of gas bearing supported turbocompressors for vapor compression cycles

机译:蒸汽压缩循环轴承支撑涡轮压缩机的尺度限制

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An analysis of single-stage centrifugal compressors supported on dynamic, gas lubricated bearings for driving vapor compression cycles suggests that the maximum feasible compressor power is limited, primarily by the bearing load capacity, in the range from 80 kW to 250 kW. The analysis further suggests that the maximum feasible compressor power depends significantly on working fluid selection. Low-pressure fluids result in large impellers with good efficiency but heavy machines, the power of which is limited by the bearing load capacity. High-pressure fluids require small machines rotating at high speeds, the power of which is limited by the rotordynamic eigenfrequencies. Consequently, there is a family of fluids that allows maximization of the power range of gas bearing supported turbocompressors. Finally, the analysis suggests that the maximum compressor power can be expressed as a function of the reduced evaporation pressure, regardless of the working fluid choice. Maximum COP is reached at a reduced evaporation pressure decreasing nearly linearly from 0.22 to 0.11 as the temperature lift between the evaporator and the condenser increases from 20 K to 50 K. The feasible maximum compressor power increases with increasing specific compressor speed, bearing tip speed (NDm) and rotordynamic stability safety margin. (C) 2019 Elsevier Ltd and IIR. All rights reserved.
机译:用于驱动蒸汽压缩循环的动态,气体润滑轴承支撑的单级离心压缩机的分析表明,最大可行压缩机功率主要受限,主要是轴承载荷容量,范围为80千瓦至250千瓦。该分析进一步表明,最大可行压缩机功率取决于工作流体选择。低压流体导致具有良好效率但重型机器的大型叶轮,其功率受到轴承承载能力的限制。高压液需要高速旋转的小机器,其功率受到旋转动力学特征频道的限制。因此,存在一系列流体,其允许最大化气体支撑的涡轮压缩机的功率范围。最后,分析表明,无论工作流体选择如何,最大压缩机功率都可以表示为降低的蒸发压力的函数。随着蒸发器和冷凝器之间的温度升力从20k到50k增加,在0.22至0.11的蒸发压力下降几乎线性地减小的最大COP。随着特定压缩机速度的增加,可行的最大压缩机功率随着特定的压缩机速度,轴承尖端速度而增加,可行的最大压缩机功率增加,几乎线性地升高。 NDM)和旋转动力稳定性安全保证金。 (c)2019年Elsevier Ltd和IIR。版权所有。

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