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Heat-Loss Calculations in a SCWR Fuel-Channel

机译:SCWR燃料通道中的热损失计算

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The objective of this paper is to calculate heat losses from a CANDU-6 fuel-channel while modifying it according to the specified operating pressure and temperature conditions of Supercritical Water-cooled Reactors (SCWRs). Heat losses from the coolant to the moderator are significant in a SCWR because of high operating temperatures (i.e., 350 - 625°C). This has adverse effects on the overall thermal efficiency of the Nuclear Power Plant (NPP), so it is necessary to determine the amount of heat losses from fuel-channels proposed for SCWRs. Inconel-718 was chosen as a pressure tube (PT) material and PT minimum required thickness was calculated in accordance with the coolant's maximum operating pressure and temperature. The heat losses from the fuel-channel were calculated along the heated length of the fuel-channel.Steady-state one-dimensional heat-transfer analysis was conducted, and programming in MATLAB was performed. The fuel-channel was divided into small segments and for each segment thermal resistances of the fuel-channel components were analyzed. Further, the thermophysical properties of the coolant, annulus gas, and moderator were retrieved from the NIST REFPROP software. The analysis outcome resulted in a total heat loss of 29.3 kW per fuel-channel when the pressure of the annulus gas was 0.3 Mpa.
机译:本文的目的是计算CANDU-6燃料通道的热损失,同时根据超临界水冷堆(SCWR)的指定工作压力和温度条件对其进行修改。由于较高的工作温度(即350至625°C),在SCWR中从冷却剂到减速剂的热损失非常大。这对核电厂(NPP)的整体热效率有不利影响,因此有必要确定为SCWR设计的燃料通道的热量损失量。选择Inconel-718作为压力管(PT)的材料,并根据冷却液的最大工作压力和温度计算PT所需的最小厚度。沿着燃料通道的加热长度计算出燃料通道的热损失。 进行稳态一维传热分析,并在MATLAB中进行编程。将燃料通道分成小段,并针对每个段分析燃料通道组件的热阻。此外,还可以从NIST REFPROP软件中获取冷却液,环空气体和调节剂的热物理性质。当环空气体的压力为0.3 Mpa时,分析结果导致每个燃料通道的总热损失为29.3 kW。

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