空间气冷反应堆堆芯流动换热数值仿真研究

Numerical Study of Flow and Heat Transfer Characteristic of Space Gas-cooled Nuclear Reactor Core

  • 摘要: 以美国普罗米修斯计划反应堆为参考,建立了空间气冷反应堆堆芯结构的三维模型,利用蒙特卡罗方法计算得到了堆芯真实功率分布,并使用Star-CCM+软件开展了1/6堆芯的流动换热计算,分析得到了堆芯温度场、速度场和压力场的分布情况,评估了现有设计中仍待优化之处,并提出了相关的优化建议。计算结果表明,该反应堆设计可将冷却剂加热到工作温度,能满足基本的技术指标。但从优化角度考虑,需对堆芯入口段与出口段进行优化设计,通过改变入口管与压力容器间的角度等,可降低不必要的能量损失,提高堆芯出口温度与速度分布均匀性,同时降低冷却剂对诸如气轮机等设备的不利影响。

     

    Abstract: The Prometheus project reactor was modeled as a prototype and numerical analysis using CFD software was also conducted. The power profile of the reactor core was obtained by the Monte Carlo method and the thermal-hydraulic simulation of one-sixth of the reactor was conducted by using the Star-CCM+ software. The temperature field, velocity field and pressure field were acquired and possible optimization suggestions were proposed based on the evaluation of the current model. It is shown that the coolant in the reactor design can be heated up to the design temperature and the main technology requirements can be satisfied. However, optimization is still needed in the reactor inlet and outlet region from the perspective of optimization. The direction of inlet nozzle can be changed to reduce unnecessary loss and increase the uniformity of temperature and velocity field at the outlet. Meanwhile, negative effects of the coolant on the turbine and other equipment are also reduced.

     

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