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Experimental evaluation of a novel solar receiver for a micro gas- turbine based solar dish system in the KTH high-flux solar simulator

机译:KTH高通量太阳模拟器中基于微型燃气轮机的太阳能碟形系统的新型太阳能接收器的实验评估

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This work presents the experimental evaluation of a novel pressurized high-temperature solar air receiver for the integration into a micro gas-turbine solar dish system reaching an air outlet temperature of 800 degrees C. The experiments are conducted in the controlled environment of the KTH high-flux solar simulator with well-defined radiative boundary conditions. Special focus is placed on providing detailed information to enable the validation of numerical models. The solar receiver performance is evaluated for a range of operating points and monitored using multiple point measurements. The porous absorber front surface temperature is measured continuously as it is one of the most critical components for the receiver performance and model validation. Additionally, pyrometer line measurements of the absorber and glass window are taken for each operating point. The experiments highlight the feasibility of volumetric solar receivers for micro gas-turbine based solar dish systems and no major hurdles were found. A receiver efficiency of 84.8% was reached for an air outlet temperature of 749 degrees C. When using a lower mass flow, an air outlet temperature of 800 degrees C is achieved with a receiver efficiency of 69.3%. At the same time, all material temperatures remain below permissible limits and no deterioration of the porous absorber is found. (C) 2018 Elsevier Ltd. All rights reserved.
机译:这项工作提出了一种新颖的加压高温太阳空气接收器的实验评估,该接收器可以集成到达到800摄氏度出气温度的微型燃气轮机太阳皿系统中。该实验是在KTH high的受控环境中进行的具有明确的辐射边界条件的-flux太阳模拟器。特别着重于提供详细的信息以使数值模型能够得到验证。针对一系列工作点评估太阳能接收器的性能,并使用多点测量对其进行监控。多孔吸收体的前表面温度是连续测量的,因为它是接收器性能和模型验证的最关键组成部分之一。另外,对每个工作点进行吸收器和玻璃窗的高温计线测量。实验强调了容积式太阳能接收器在基于微型燃气轮机的太阳能碟系统中的可行性,并且没有发现重大障碍。空气出口温度为749摄氏度时,接收器效率达到84.8%。当使用较低的质量流量时,空气接收器温度为69.3%时,空气出口温度达到800摄氏度。同时,所有材料的温度都保持在允许的极限之下,并且没有发现多孔吸收剂的劣化。 (C)2018 Elsevier Ltd.保留所有权利。

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