太阳能混合动力微型燃气轮机改进建模与实验评估

Chaz Fenner, S. J. van der Spuy
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引用次数: 0

摘要

这项研究有助于正在进行的研究,开发一种基于涡轮增压器的双轴微型燃气轮机(MGT),用于商业化的太阳能混合动力系统。本研究开发了一个改进的模型来预测MGT的性能,该模型由两个涡轮增压器组成,其中一个涡轮增压器代表燃气发电机涡轮,另一个更大的涡轮增压器用作动力涡轮单元。它通过包括通过一维热阻网络(1-D TRN)的传热影响来确定绝热出口温度,并通过考虑假定的不完全燃烧来做到这一点。总的来说,模型的温度估计与实测值的最大偏差在5%以内,压力的最大偏差在8%以内。燃烧室出口温度估计大大提高到测量值的4%以内,比以前的工作提高了15%。尽管提高了精度,但该模型仅用于较小的燃气发电机涡轮。较大功率的涡轮机被认为没有达到热平衡,因为温度估计值与实测值的偏差大大增加。随后对该设施进行的能源审计证明了1-D TRN的实用性。其结果被用来确定传热的尺度。结果表明,动力涡轮机实际上在其最佳范围外运行,导致燃气通过涡轮机的热损失率大于其产生的功率。燃烧模型的有用性也被强调为一种估计燃烧室出口温度的技术,具有可接受的精度水平,并且由于其简单性而具有快速的周转时间。1-D TRN被证明可以准确地估计MGT中的热流,尽管采用了没有为机器开发的传热系数的相关性。通过与标准装置的对比测试,发现降低寄生压力损失是提高MGT性能的重要手段。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Improved Modeling and Experimental Evaluation of a Micro Gas Turbine for Solar-Hybrid Application
This study contributes to the ongoing research to develop a turbocharger based dual-shaft Micro Gas Turbine (MGT) for a commercialized solar-hybrid system. The work in this study developed an improved model to predict the performance of the MGT which comprises of two turbochargers, with one turbocharger representing the gas generator turbine and the other, bigger turbocharger used as the power turbine unit. It did so by including the effects of heat transfer through a One-Dimensional Thermal Resistance Network (1-D TRN) to determine diabatic outlet temperatures and by accounting for the supposed incomplete combustion. Overall, the model’s temperature estimations were found to be within a maximum deviation of 5 % of the measured values and, 8 % for pressure. Combustor outlet temperature estimates were substantially improved to within 4 % of the measured value, which is a 15 % improvement on previous work. Despite the increased accuracy, the model was only validated for the smaller gas generator turbine. The larger power turbine was reasoned to have not reached thermal equilibrium as temperature estimates had substantially increased levels of deviation from the measured values. A subsequent energy audit of the facility demonstrated the utility of the 1-D TRN. The results of which were used to determine the scale of the heat transfer. It showed that the power turbine is in fact operating outside of its optimal range which resulted in the heat loss rate of the gas through the turbine being greater than the power it produced. The usefulness of the combustion model is also highlighted as a technique to estimate the combustor outlet temperature with acceptable levels of accuracy and with a rapid turn-around time due to its simplicity. The 1-D TRN was shown to estimate heat flows in the MGT accurately despite employing correlations for the heat transfer coefficients that were not developed for the machines. A combustor designed for solarized operation was benchmarked against a standard unit and the results indicated the significance of reducing parasitic pressure losses as a means to improve MGT performance.
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