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首页> 外文期刊>Applied thermal engineering: Design, processes, equipment, economics >Thermal performance of a solar high temperature thermochemical reactor powered by a solar simulator
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Thermal performance of a solar high temperature thermochemical reactor powered by a solar simulator

机译:由太阳模拟器提供动力的太阳能高温热化学反应器的热性能

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Solar thermochemical reactor is the key to store solar energy as chemical basic fuels through high temperature chemical reactions. The thermal performance of a solar high temperature thermochemical reactor coupling heat pipe technology has been preliminary performed under a high-flux solar simulator. The radiative power of the solar simulator was measured and calibrated with an infrared camera and an optical meter. The measurement indicates an average heat flux exceeding 130 kW/m(2) over a 210-mm-diameter focal plane. The temperature characteristics and thermal performance of the reactor with only nitrogen cooling were investigated under various nitrogen flow rates and heat flux inputs. It is showed that the input heat flux has effect on the reactor temperature and the temperature distribution on heating surface is associated with the radiative flux distribution from the solar simulator. The heating surface temperature is at the range of 850-1075 K for the input heat flux of 55.5-108.8 kW/m2 and cooling gas flow rate less than 33 m(3)/h. The gas out temperature obtained is lower than 700 K with room temperature inlet. The radiation heat loss through heating surface accounts for 45-60% of the radiative power incident on the reactor. The thermal efficiency of STPCR is greatly influenced by cooling gas flow rate and it is in the range of 27-90% with cooling gas flow rate from 5 m(3)/h to 33 m(3)/h. Whereas the thermal efficiency appears less influenced by heat flux inputs. Good heat absorbing and transfer abilities of the reactor has been shown.
机译:太阳能热化学反应器是通过高温化学反应将太阳能作为化学碱性燃料存储太阳能的关键。在高磁通太阳能模拟器下,太阳能高温热化学反应器耦合热管技术的热性能已经初步进行。测量太阳模拟器的辐射功率并用红外相机和光学计校准。测量表明在210mm直径的焦平面上超过130kW / m(2)的平均热通量。在各种氮气流速下,研究了反应器的温度特性和热性能,并在各种氮流速和热通量输入下进行了研究。结果表明,输入热通量对反应器温度有影响,加热表面上的温度分布与来自太阳模拟器的辐射助焊剂分布相关。加热表面温度为850-1075k,输入热通量为55.5-108.8 kW / m 2,冷却气体流速小于33 m(3)/ h。获得的气体温度低于700 k,室温入口低700 k。通过加热表面的辐射热损失占反应器上入射的辐射功率的45-60%。 STPCR的热效率受到冷却气体流速的大大影响,并且在27-90%的范围内,冷却气体流速从5米(3)/ h至33μm(3)/ h。而热效率似乎对热通量输入的影响较小。已经显示了反应器的良好吸热和转移能力。

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